command: ./cs_solver *************************************************************** (R) Code_Saturne Version 7.1-alpha Copyright (C) 1998-2021 EDF S.A., France build Thu 20 May 2021 17:48:42 BST 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: Sat 22 May 2021 16:04:50 BST System: Linux 5.4.0-73-generic (Ubuntu 18.04.5 LTS) Machine: CLWS00114 Processor: model name : Intel(R) Xeon(R) Bronze 3104 CPU @ 1.70GHz Memory: 31769 MB User: ruonanwang (Ruonan Wang) Directory: /home/ruonanwang/cases/20210522_Northrop_adiabatic_energy_equation_Re2E7/wrrans/RESU/20210522-1604 OpenMP threads: 3 Processors/node: 6 Compilers used for build: C compiler: gcc (Ubuntu 7.5.0-3ubuntu1~18.04) 7.5.0 C++ compiler: g++ (Ubuntu 7.5.0-3ubuntu1~18.04) 7.5.0 Fortran compiler: GNU Fortran (Ubuntu 7.5.0-3ubuntu1~18.04) 7.5.0 MPI version: 3.1 (Open MPI 2.1.1) I/O read method: standard input and output, serial access I/O write method: standard input and output, serial access External libraries for partitioning: ParMETIS 4.0.3 PT-SCOTCH 6.1.0 =============================================================== CALCULATION PREPARATION ======================= =========================================================== @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ @ @@ WARNING: IN THE DATA SPECIFICATION @ ======== @ @ The k-omega turbulence model has been chosen. In order to @ have a correct calculation restart, the ICDPAR indicator @ has been set to 1 (read the wall distance in the restart @ file). @ If this initialization raises any issue (modification of, @ the number and position of the wall faces since the @ previous calcuation), force ICDPAR=1 (there might be, @ a small shift in the turbulent viscosity at the, @ first time-step)., @ @ The calculation will be run. @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ No error detected during the data verification cs_user_parameters.f90 and others). =========================================================== CALCULATION PARAMETERS SUMMARY ============================== ----------------------------------------------------------- ** DIMENSIONS ---------- --- Physics NVAR = 9 (Nb variables ) NSCAL = 2 (Nb scalars ) NSCAUS = 0 (Nb user scalars ) NSCAPP = 2 (Nb specific physics scalars ) ----------------------------------------------------------- ** HOMOGENEOUS MIXTURE MODEL VoF ---------------------------------------- IVOFMT = 0 ( 0 : disabled ) ( > 0: enabled ) ----------------------------------------------------------- ** COMPRESSIBLE: additional data ------------ --- Continuous phase : ICV = -1 (0: Cv cst; 1: variable ) IVISCV = -1 (0: kappa cst; 1: variable kappa: volume viscosity in kg/(m.s) ) VISCV0 = 0.00000E+00 (kappa value if constant ) ICFGRP = 1 (1: pressure BC with dominant hydrostatic effect ) ----------------------------------------------------------- ** TIME STEPPING ------------- --- Per-variable properties ------------------------------------ Variable ISTAT CDTVAR ------------------------------------ Velocity 1 0.1000E+01 Pressure 1 0.1000E+01 k 1 0.1000E+01 omega 1 0.1000E+01 TotEner 1 0.1000E+01 temperature 1 0.1000E+01 Wall distance 0 0.1000E+01 ---------------------------- ISTAT = 0 ou 1 (1 for unsteady ) CDTVAR > 0 (time step multiplier ) --- Order of base time stepping scheme ISCHTP = 1 (1: order 1; 2: order 2 ) ----------------------------------------------------------- ** STOKES ------ -- Continuous phase: ISTMPF = 1 (time scheme for flow (0: explicit (THETFL = 0 ) (1: std scheme (Saturne 1.0 ) (2: 2nd-order (THETFL = 0.5 ) THETVI = 0.00000E+00 (theta for total viscosity ((1+theta).new-theta.old THETCP = -0.99900E+03 (specific heat theta-scheme ((1+theta).new-theta.old THETSN = 0.00000E+00 (Nav-Stokes S.T. theta scheme) ((1+theta).new-theta.old THETST = 0.00000E+00 (Turbulence S.T. theta-scheme) ((1+theta).new-theta.old EPSUP = 0.10000E-04 (Velocity/pressure coupling stop test ) ----------------------------------------------------------- ** WALL DISTANCE COMPUTATION ------------------------- ICDPAR = 1 ( 1: std, reread if restart (-1: std, recomputed if restrt ( 2: old, reread if restart (-2: old, recomputed if restrt ----------------------------------------------------------- ** SCALARS ------- ITBRRB = 0 (T or H reconstruction at bdy) ----------------------------------------------------- Variable Number ITURT ----------------------------------------------------- TotEner 1 0 temperature 2 0 ------------------------------------------------------------- ------------------------------------ Variable Number RVARFL ------------------------------------ TotEner 1 0.8000E+00 temperature 2 0.8000E+00 ------------------------------------------- ------------------------------------------------------- Variable Number ICLVFL SCAMIN SCAMAX ------------------------------------------------------- TotEner 1 -1 -0.1000E+13 0.1000E+13 temperature 2 -1 -0.1000E+13 0.1000E+13 ------------------------------------------------------- ------------------------------------------------------------- For each scalar, the number indicates it's rank in the list of all scalars. User scalars are placed first, from 1 to NSCAUS. Specific physics scalars are placed at the end, from NSCAUS+1 to NSCAPP+NSCAUS=NSCAL. is_temerature = 0 or 1 (use Cp or not ) VISLS0 = >0 (Reference viscosity ) SIGMAS = >0 (Schmidt ) RVARFL = >0 (Rf, cf variance dissipation ) ICLVFL = 0, 1 or 2 (Variance clipping mode ) SCAMIN = (Min authorized value ) SCAMAX = (Max authorized value ) For variances, SCAMIN is ignored and SCAMAX is used only if ICLVFL = 2 ------------------------------------------------------ Scalar THETSS THETVS ------------------------------------------------------ 1 0.0000E+00 0.0000E+00 2 0.0000E+00 0.0000E+00 ------------------------------------------------------ THETSS = (theta for source terms ) ((1+theta).new-theta.old ) THETVS = (theta for scalar diffusivity ((1+theta).new-theta.old ) ----------------------------------------------------------- ** CALCULATION MANAGEMENT ---------------------- --- Restarted calculation ISUITE = 1 (1: restarted calculation ) ILEAUX = 1 (1: read restart/auxiliary ) IECAUX = 1 (1: write checkpoint/auxiliary) --- Calculation time The numbering of time steps and the measure of simulated physical time are absolute values, and not values relative to the current calculation. NTPABS = 30000 (Initial time step) NTMABS = 500000 (Final time step required) ----------------------------------------------------------- ** INPUT-OUTPUT ------------ --- Restart file NTSUIT = 1000 (Checkpoint frequency ) --- Probe history files NTHIST = 1 (Output frequency ) FRHIST = -.10000E+01 (Output frequency (s) ) -- -- -- --- run_solver.log files NTLIST = 1 (Output frequency ) -- -- -- --- Additional post-processing variables (ipstdv) ipstfo = 7 (Force exerted by the fluid on the boundary) ipstyp = 1 (y+ at boundary) ipsttp = 1 (T+ at boundary) ipstft = 1 (Thermal flux at boundary) ipstnu = 1 (Dimensionless thermal flux at boundary) ----------------------------------------------------------- ** ALE METHOD (MOVING MESH) ----------- IALE = 0 (1: activated,2: CDO ) NALINF = 0 (Fluid initialization iterations) IFLXMW = 0 (ALE mass flux computation 0: thanks to vertices 1: thanks to mesh velocity) ----------------------------------------------------------- Postprocessing output writers: ------------------------------ -1: name: results directory: postprocessing format: EnSight Gold options: separate_meshes time dependency: fixed mesh output: every 360 time steps, at end -5: name: directory: monitoring format: time_plot options: CSV time dependency: fixed mesh output: every time step -6: name: directory: profiles format: plot options: time dependency: fixed mesh output: at end -7: name: histograms directory: histograms format: histogram options: txt time dependency: fixed mesh output: at end Reading file: restart/mesh_input.csm Finished reading: restart/mesh_input.csm ---------------------------------------------------------- Composing periodicities Halo construction with standard neighborhood ============================================ Face interfaces creation Definition of periodic vertices Vertex interfaces creation Halo creation Halo definition Local halo definition Distant halo creation Updating the faces -> cells connectivity Number of cells: 50160 ---------------------------------------------------------- Number of cells + halo cells: 75240 ---------------------------------------------------------- Number of ghost cells: 25080 ---------------------------------------------------------- Number of interior faces: 162032 ---------------------------------------------------------- Number of boundary faces: 1976 ---------------------------------------------------------- Histogram of the number of interior faces per cell: minimum value = 4 maximum value = 6 1 : [ 4 ; 5 [ = 24 2 : [ 5 ; 6 ] = 50136 ---------------------------------------------------------- Synchronizing cell families Renumbering mesh: renumbering for cells: pre-numbering: no renumbering cells adjacent to ghost cells last: no numbering: no renumbering renumbering for interior faces: cell adjacency pre-ordering: lowest id first faces adjacent to ghost cells last: no numbering: multipass renumbering for boundary faces: numbering: no shared cell across threads renumbering for vertices: numbering: no renumbering Numbering for cells: type: default number of halo-adjacent elements: 50160 Numbering for interior faces: type: threads number of threads: 3 number of exclusive groups: 3 number of elements in group 0: 138085 number of elements in group 1: 23946 number of elements in group 2: 1 estimated thread imbalance: 0.413 Numbering for boundary faces: type: threads number of threads: 3 number of exclusive groups: 1 number of elements in group 0: 1976 estimated thread imbalance: 0.001 ---------------------------------------------------------- Matrix bandwidth for volume mesh : 62400 Matrix profile/lines for volume mesh : 19028 Mesh coordinates: minimum and maximum X : -1.8545362e-16 5.9000000e-02 Y : -3.7785899e-03 3.7785899e-03 Z : 7.5997106e-02 4.3300003e-01 Mesh Number of cells: 50160 Number of interior faces: 162032 Number of boundary faces: 1976 Number of vertices: 63940 Periodic faces (which are also interior faces): Periodicity 1: 12540 face couples Groups: "DISC_DOWNSTREAM" boundary faces: 400 "DISC_UPSTREAM" boundary faces: 400 "EXTEND_DOWNSTREAM" boundary faces: 108 "EXTEND_UPSTREAM" boundary faces: 108 "INLET" boundary faces: 480 "Northrop and Owen for wmles one" cells: 50160 interior faces: 25080 boundary faces: 1976 "OUTLET" boundary faces: 80 "PER1" interior faces: 12540 "PER2" interior faces: 12540 "SHROUD_DOWNSTREAM" boundary faces: 200 "SHROUD_UPSTREAM" boundary faces: 200 --- Information on the volumes Minimum control volume = 1.8674660e-15 Maximum control volume = 2.4932839e-08 Total volume for the domain = 9.1379646e-05 Criterion 1: Orthogonality: Number of bad cells detected: 0 --> 0 % Criterion 2: Offset: Number of bad cells detected: 0 --> 0 % Criterion 3: Least-Squares Gradient Quality: Number of bad cells detected: 0 --> 0 % Criterion 4: Cells Volume Ratio: Number of bad cells detected: 0 --> 0 % Criterion 5: Guilt by Association: Number of bad cells detected: 0 --> 0 % Computing geometric quantities (0.111 s) --- Information on volume zones Volume zone "cells" id = 0 Number of cells = 50160 Volume = 9.138e-05 Center of gravity = (0.0295, -2.13e-19, 0.29302) Surface = -1 (not computed) Volume zone "all_cells" id = 1 Number of cells = 50160 Volume = 9.138e-05 Center of gravity = (0.0295, -2.13e-19, 0.29302) Surface = -1 (not computed) --- Information on boundary zones Boundary zone "boundary_faces" id = 0 Number of faces = 1976 Surface = 0.0036906 Center of gravity = (0.0295, 1.1977e-16, 0.30731) Perimeter = -1 (not computed) Boundary zone "BC_1" id = 1 Number of faces = 400 Surface = 0.0015482 Center of gravity = (0.059, 1.3807e-16, 0.29297) Perimeter = -1 (not computed) Boundary zone "BC_2" id = 2 Number of faces = 400 Surface = 0.0015482 Center of gravity = (1.7948e-16, 1.3835e-16, 0.29297) Perimeter = -1 (not computed) Boundary zone "BC_3" id = 3 Number of faces = 108 Surface = 3.7568e-05 Center of gravity = (0.03, 1.9368e-16, 0.4305) Perimeter = -1 (not computed) Boundary zone "BC_4" id = 4 Number of faces = 108 Surface = 3.7568e-05 Center of gravity = (0.029, 1.94e-16, 0.4305) Perimeter = -1 (not computed) Boundary zone "BC_5" id = 5 Number of faces = 480 Surface = 7.826e-05 Center of gravity = (0.0295, 2.7112e-20, 0.075999) Perimeter = -1 (not computed) Boundary zone "BC_6" id = 6 Number of faces = 80 Surface = 7.5573e-06 Center of gravity = (0.0295, -2.4969e-18, 0.43299) Perimeter = -1 (not computed) Boundary zone "BC_7" id = 7 Number of faces = 200 Surface = 0.00021663 Center of gravity = (0.0445, -1.2089e-18, 0.42799) Perimeter = -1 (not computed) Boundary zone "BC_8" id = 8 Number of faces = 200 Surface = 0.00021663 Center of gravity = (0.0145, -1.235e-18, 0.42799) Perimeter = -1 (not computed) Probe set: "probes": maximum distance between cell centers and requested coordinates: 4.904e-06 ALMAX = 0.45042E-01 (Characteristic length ) ALMAX is the cubic root of the domain volume. ALMAX is the length used to initialize the turbulence. -------------------------------------------------------------------------------- ----------------------------------------------------------- ** READING MAIN AND AUXILIARY RESTART FILES ---------------------------------------- READING THE MAIN RESTART FILE Start reading Reading dimensions complete Reading the previous time step number (restarting computation) NTPABS = 30000 Reading the previous time step number (restarting computation) TTPABS = 0.1587E-01 Reading options complete Read variables from restart: restart/main.csc Reading complete READING THE AUXILIARY RESTART FILE Start reading Finished reading options restart/auxiliary.csc: section "ref_presstot01" not present. @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ @ @@ WARNING: WHEN READING THE AUXILIARY RESTART FILE @ ======= @ Lecture des proprietes physiques @ @ It was not possible to read some values from the @ auxiliary restart file. @ They will be initialized by the default values. @ @ This situation can occur when the restart file @ originates from a run realised with different @ options or when the file is damaged. @ @ The run will continue... @ @@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@ @ Fin de la lecture des proprietes physiques Fin de la lecture du pas de temps Fin de la lecture des flux de masse Fin de la lecture des conditions aux limites restart/auxiliary.csc: section "time_moments:sizes" not present. Fin de la lecture de la distance a la paroi End reading ----------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Property Min. value Max. value ----------------------------------------- density 0.4572E+00 0.4326E+01 molecular_viscos 0.1810E-04 0.1810E-04 turbulent_viscos 0.9081E-18 0.6413E-01 ----------------------------------------- --- Diffusivity: ----------------------------------------------- Scalar Number Min. value Max. value ----------------------------------------------- TotEner 1 0.3607E-04 0.3607E-04 temperature 2 0.2590E-01 0.2590E-01 ----------------------------------------------- ** INFORMATION ON BOUNDARY FACES TYPE ---------------------------------- ------------------------------------------------------------------------- Boundary type Code Nb faces ------------------------------------------------------------------------- Sub. enth. inlet 11 0 Ptot, Htot 10 0 Imp inlet/outlet 7 480 Subsonic outlet 9 0 Supersonic outlet 8 0 Smooth wall 5 1416 Rough wall 6 0 Symmetry 4 0 Undefined 1 0 User type 3 80 ------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ----------- -------------- -------------- ------------ ------------ a TotEner a temperature ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -196.37 196.37 0.0014566 0.00045629 v Velocity[Y] -0.1307 701.89 250.37 80.875 v Velocity[Z] -19.272 333.54 23.361 1.9387 v ǁVelocityǁ 0.077065 701.9 258.93 83.621 v Pressure 60425 1.1023e+05 1.0389e+05 1.0417e+05 v k 1.2199e-08 40625 900.08 355.54 v omega 153.55 9.6797e+09 1.8455e+08 3.414e+05 v TotEner 99212 6.2954e+05 3.4147e+05 2.4848e+05 v temperature 73.093 533.96 398.42 337.14 v Density 0.4572 4.3259 0.95084 1.0905 v TurbVisc 9.0808e-19 0.064129 0.010064 0.028616 v CourantNb 0 0 0 0 v FourierNb 0 0 0 0 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 73.093 533.96 404.7 422.14 v Boundary Density 0.4572 4.3259 0.98517 0.8972 v Yplus 0 0 0 0 =============================================================== MAIN CALCULATION ================ =============================================================== =============================================================== INSTANT 0.158672783E-01 TIME STEP NUMBER 30001 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.597816137E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560817608E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123522691E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10381E+01 0.55688E+02 Friction velocity uk : 0.10381E+01 0.55688E+02 Dimensionless distance yplus : 0.20632E-01 0.42740E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14490E-01 0.12411E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60087E+03 15 0.65732E-07 0.91236E+04 0.23099E+04 c Velocity[X] 0.42607E+04 c Velocity[Y] 0.56205E+02 c Velocity[Z] 0.48067E+04 c Pressure 0.75268E-01 11 0.47822E-07 0.64097E+09 0.66631E+03 c k 0.24233E+04 1 0.97374E-06 0.18360E+06 0.21903E+04 c omega 0.81510E+09 1 0.76913E-07 0.36372E+15 0.13966E+04 c TotEner 0.24198E+06 1 0.13910E-05 0.11090E+10 0.36263E+03 c temperature 0.00000E+00 0 0.00000E+00 0.16800E+04 0.33070E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1664e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -203.06 203.06 0.0014583 0.00046 v Velocity[Y] -0.1307 701.89 250.39 80.876 v Velocity[Z] -19.271 333.6 23.457 1.9388 v ǁVelocityǁ 0.076998 701.9 258.99 83.622 v Pressure 54412 1.1027e+05 1.0388e+05 1.0417e+05 v k 1.2195e-08 40635 900.03 355.54 v omega 153.55 9.6787e+09 1.8452e+08 3.4139e+05 v TotEner 99168 6.2955e+05 3.4147e+05 2.4848e+05 v temperature 73.033 533.96 398.38 337.14 v Density 0.4266 4.3265 0.95085 1.0905 v TurbVisc 9.0808e-19 0.064129 0.010064 0.028616 v CourantNb 1.2182e-05 36.697 0.34737 0.0075683 v FourierNb 4.5255e-05 237.97 2.0264 0.090487 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 73.093 533.96 404.06 422.1 v Boundary Density 0.4572 4.3259 0.98517 0.8972 v Yplus 0 42.74 2.4903 0.95223 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7051e-05 40.062 0.43051 0.010587 INSTANT 0.158675411E-01 TIME STEP NUMBER 30002 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.598524084E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560817607E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.127815503E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10390E+01 0.55830E+02 Friction velocity uk : 0.10390E+01 0.55830E+02 Dimensionless distance yplus : 0.20654E-01 0.42743E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14506E-01 0.12412E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60087E+03 14 0.60602E-07 0.78162E+04 0.21380E+04 c Velocity[X] 0.43950E+04 c Velocity[Y] 0.22372E+02 c Velocity[Z] 0.33989E+04 c Pressure 0.75272E-01 7 0.13106E-07 0.15797E+09 0.33078E+03 c k 0.24235E+04 1 0.94329E-06 0.11261E+06 0.17152E+04 c omega 0.81509E+09 1 0.79536E-07 0.55304E+15 0.17222E+04 c TotEner 0.24199E+06 1 0.13617E-05 0.38076E+09 0.21249E+03 c temperature 0.00000E+00 0 0.00000E+00 0.46137E+03 0.17330E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.2734e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -207.67 207.67 0.0014312 0.00046367 v Velocity[Y] -0.13069 701.89 250.4 80.877 v Velocity[Z] -19.271 333.69 23.545 1.939 v ǁVelocityǁ 0.076914 701.9 259.04 83.623 v Pressure 53763 1.1027e+05 1.0388e+05 1.0417e+05 v k 1.2164e-08 40645 900.04 355.54 v omega 153.56 9.6773e+09 1.8448e+08 3.4138e+05 v TotEner 99118 6.2955e+05 3.4148e+05 2.4848e+05 v temperature 72.964 533.97 398.36 337.14 v Density 0.41914 4.3267 0.95085 1.0905 v TurbVisc 9.0814e-19 0.064129 0.010064 0.028616 v CourantNb 1.2191e-05 38.821 0.3531 0.0075689 v FourierNb 4.5252e-05 239.93 2.0235 0.090487 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 73.033 533.96 403.65 422.09 v Boundary Density 0.4266 4.3265 0.98379 0.89719 v Yplus 0 42.743 2.4665 0.95155 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7063e-05 40.224 0.43696 0.010587 INSTANT 0.158678038E-01 TIME STEP NUMBER 30003 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.596139218E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560879774E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.127673707E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10375E+01 0.55998E+02 Friction velocity uk : 0.10375E+01 0.55998E+02 Dimensionless distance yplus : 0.20627E-01 0.42743E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14487E-01 0.12412E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60087E+03 13 0.60835E-07 0.47697E+04 0.16701E+04 c Velocity[X] 0.27780E+04 c Velocity[Y] 0.15924E+02 c Velocity[Z] 0.19758E+04 c Pressure 0.75277E-01 7 0.10821E-07 0.91263E+08 0.25142E+03 c k 0.24237E+04 1 0.93510E-06 0.12735E+06 0.18240E+04 c omega 0.81508E+09 1 0.18690E-07 0.33113E+14 0.42141E+03 c TotEner 0.24199E+06 1 0.13490E-05 0.24663E+09 0.17101E+03 c temperature 0.00000E+00 0 0.00000E+00 0.37294E+03 0.15581E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.2617e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -210.59 210.59 0.0013977 0.00046732 v Velocity[Y] -0.13069 701.89 250.4 80.878 v Velocity[Z] -19.27 333.8 23.621 1.9392 v ǁVelocityǁ 0.076812 701.9 259.09 83.624 v Pressure 54684 1.1027e+05 1.0387e+05 1.0417e+05 v k 1.2137e-08 40654 900.08 355.53 v omega 153.56 9.677e+09 1.8447e+08 3.4138e+05 v TotEner 99064 6.2954e+05 3.4148e+05 2.4848e+05 v temperature 72.89 533.98 398.34 337.14 v Density 0.42459 4.3267 0.95083 1.0905 v TurbVisc 9.0602e-19 0.064129 0.010064 0.028616 v CourantNb 1.2199e-05 39.841 0.35724 0.0075696 v FourierNb 4.5249e-05 238.47 2.0068 0.090487 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.964 533.97 403.58 422.09 v Boundary Density 0.41914 4.3267 0.98348 0.89717 v Yplus 0 42.743 2.4629 0.9513 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7075e-05 40.368 0.44167 0.010587 INSTANT 0.158680666E-01 TIME STEP NUMBER 30004 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.593888322E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560907060E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.127534842E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10404E+01 0.56221E+02 Friction velocity uk : 0.10404E+01 0.56221E+02 Dimensionless distance yplus : 0.20684E-01 0.42743E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14527E-01 0.12412E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60087E+03 12 0.63291E-07 0.28693E+04 0.12954E+04 c Velocity[X] 0.15989E+04 c Velocity[Y] 0.16220E+02 c Velocity[Z] 0.12542E+04 c Pressure 0.75281E-01 8 0.95018E-08 0.71548E+08 0.22262E+03 c k 0.24240E+04 1 0.94086E-06 0.15386E+06 0.20047E+04 c omega 0.81508E+09 1 0.16629E-07 0.26304E+14 0.37560E+03 c TotEner 0.24199E+06 1 0.13405E-05 0.18044E+09 0.14628E+03 c temperature 0.00000E+00 0 0.00000E+00 0.31901E+03 0.14411E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.2524e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -212.54 212.54 0.0013799 0.00047101 v Velocity[Y] -0.13068 701.89 250.4 80.879 v Velocity[Z] -19.269 333.93 23.687 1.9394 v ǁVelocityǁ 0.076693 701.9 259.13 83.625 v Pressure 55193 1.1027e+05 1.0387e+05 1.0417e+05 v k 1.2109e-08 40661 900.15 355.53 v omega 153.57 9.677e+09 1.8447e+08 3.4138e+05 v TotEner 99010 6.2954e+05 3.4149e+05 2.4848e+05 v temperature 72.816 533.99 398.32 337.15 v Density 0.42906 4.3266 0.9508 1.0905 v TurbVisc 9.0403e-19 0.064129 0.010064 0.028616 v CourantNb 1.2207e-05 40.312 0.36028 0.0075702 v FourierNb 4.5246e-05 236.62 1.9921 0.090487 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.89 533.98 403.61 422.09 v Boundary Density 0.42459 4.3267 0.98343 0.89717 v Yplus 0 42.743 2.4637 0.95124 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7086e-05 40.484 0.44526 0.010588 INSTANT 0.158683293E-01 TIME STEP NUMBER 30005 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.591769567E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560939094E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.127399332E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10414E+01 0.56397E+02 Friction velocity uk : 0.10414E+01 0.56397E+02 Dimensionless distance yplus : 0.20704E-01 0.42742E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14541E-01 0.12412E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60087E+03 11 0.67456E-07 0.19373E+04 0.10644E+04 c Velocity[X] 0.97950E+03 c Velocity[Y] 0.17780E+02 c Velocity[Z] 0.94001E+03 c Pressure 0.75285E-01 8 0.92580E-08 0.59511E+08 0.20303E+03 c k 0.24242E+04 1 0.94905E-06 0.16473E+06 0.20742E+04 c omega 0.81508E+09 1 0.15400E-07 0.20877E+14 0.33462E+03 c TotEner 0.24199E+06 1 0.13348E-05 0.13011E+09 0.12421E+03 c temperature 0.00000E+00 0 0.00000E+00 0.24567E+03 0.12646E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.2443e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -213.89 213.89 0.0013793 0.00047475 v Velocity[Y] -0.13068 701.89 250.41 80.88 v Velocity[Z] -19.269 334.03 23.743 1.9395 v ǁVelocityǁ 0.076558 701.9 259.16 83.626 v Pressure 55306 1.1027e+05 1.0386e+05 1.0417e+05 v k 1.2083e-08 40667 900.23 355.53 v omega 153.57 9.6771e+09 1.8447e+08 3.4138e+05 v TotEner 98955 6.2954e+05 3.4149e+05 2.4848e+05 v temperature 72.741 533.99 398.31 337.15 v Density 0.42916 4.3265 0.95076 1.0905 v TurbVisc 9.0196e-19 0.064129 0.010064 0.028616 v CourantNb 1.2215e-05 40.567 0.36261 0.0075708 v FourierNb 4.5243e-05 235.68 1.9842 0.090487 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.816 533.99 403.66 422.09 v Boundary Density 0.42906 4.3266 0.98345 0.89717 v Yplus 0 42.742 2.465 0.95125 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7098e-05 40.585 0.44807 0.010589 INSTANT 0.158685921E-01 TIME STEP NUMBER 30006 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.589781094E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560973715E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.127267573E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10415E+01 0.56526E+02 Friction velocity uk : 0.10415E+01 0.56526E+02 Dimensionless distance yplus : 0.20705E-01 0.42742E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14542E-01 0.12412E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60088E+03 10 0.72021E-07 0.13984E+04 0.90431E+03 c Velocity[X] 0.59697E+03 c Velocity[Y] 0.18848E+02 c Velocity[Z] 0.78261E+03 c Pressure 0.75289E-01 7 0.10209E-07 0.53376E+08 0.19228E+03 c k 0.24244E+04 1 0.95808E-06 0.16541E+06 0.20784E+04 c omega 0.81508E+09 1 0.13381E-07 0.14979E+14 0.28343E+03 c TotEner 0.24199E+06 1 0.13309E-05 0.97947E+08 0.10777E+03 c temperature 0.00000E+00 0 0.00000E+00 0.18998E+03 0.11121E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.2358e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -214.85 214.85 0.001389 0.00047855 v Velocity[Y] -0.13067 701.89 250.41 80.881 v Velocity[Z] -19.268 334.07 23.792 1.9397 v ǁVelocityǁ 0.076405 701.9 259.19 83.627 v Pressure 55232 1.1027e+05 1.0385e+05 1.0417e+05 v k 1.206e-08 40672 900.31 355.53 v omega 153.58 9.6771e+09 1.8448e+08 3.4138e+05 v TotEner 98902 6.2954e+05 3.4149e+05 2.4849e+05 v temperature 72.669 533.99 398.3 337.15 v Density 0.42851 4.3265 0.95072 1.0905 v TurbVisc 9.0003e-19 0.064129 0.010064 0.028617 v CourantNb 1.2224e-05 40.724 0.36444 0.0075714 v FourierNb 4.524e-05 235.88 1.9814 0.090489 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.741 533.99 403.71 422.09 v Boundary Density 0.42916 4.3265 0.98347 0.89717 v Yplus 0 42.742 2.4659 0.95128 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7109e-05 40.692 0.45036 0.010589 INSTANT 0.158688548E-01 TIME STEP NUMBER 30007 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.587920831E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561007013E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.127139914E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10412E+01 0.56620E+02 Friction velocity uk : 0.10412E+01 0.56620E+02 Dimensionless distance yplus : 0.20700E-01 0.42741E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14538E-01 0.12412E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60088E+03 9 0.76078E-07 0.10200E+04 0.77230E+03 c Velocity[X] 0.31887E+03 c Velocity[Y] 0.18968E+02 c Velocity[Z] 0.68212E+03 c Pressure 0.75293E-01 6 0.99853E-08 0.50639E+08 0.18728E+03 c k 0.24245E+04 1 0.96634E-06 0.17283E+06 0.21243E+04 c omega 0.81508E+09 1 0.11853E-07 0.11002E+14 0.24291E+03 c TotEner 0.24199E+06 1 0.13276E-05 0.80019E+08 0.97409E+02 c temperature 0.00000E+00 0 0.00000E+00 0.15589E+03 0.10074E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.2248e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -215.56 215.55 0.0014043 0.00048237 v Velocity[Y] -0.13067 701.89 250.41 80.882 v Velocity[Z] -19.268 334.02 23.836 1.9399 v ǁVelocityǁ 0.076236 701.9 259.22 83.627 v Pressure 55163 1.1027e+05 1.0385e+05 1.0417e+05 v k 1.204e-08 40675 900.38 355.53 v omega 153.58 9.6772e+09 1.8448e+08 3.4138e+05 v TotEner 98850 6.2954e+05 3.415e+05 2.4849e+05 v temperature 72.598 533.99 398.29 337.15 v Density 0.42769 4.3265 0.95068 1.0905 v TurbVisc 8.9829e-19 0.064129 0.010064 0.028617 v CourantNb 1.2238e-05 40.829 0.36592 0.0075719 v FourierNb 4.5237e-05 237.05 1.9817 0.09049 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.669 533.99 403.75 422.09 v Boundary Density 0.42851 4.3265 0.98347 0.89717 v Yplus 0 42.741 2.4664 0.95132 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.712e-05 40.83 0.45225 0.01059 INSTANT 0.158691176E-01 TIME STEP NUMBER 30008 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.586186724E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561036624E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.127016660E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10410E+01 0.56690E+02 Friction velocity uk : 0.10410E+01 0.56690E+02 Dimensionless distance yplus : 0.20695E-01 0.42742E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14535E-01 0.12412E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60088E+03 8 0.79668E-07 0.77309E+03 0.67237E+03 c Velocity[X] 0.14847E+03 c Velocity[Y] 0.18261E+02 c Velocity[Z] 0.60636E+03 c Pressure 0.75297E-01 6 0.85329E-08 0.47085E+08 0.18059E+03 c k 0.24247E+04 1 0.97154E-06 0.19587E+06 0.22614E+04 c omega 0.81509E+09 1 0.10616E-07 0.84015E+13 0.21227E+03 c TotEner 0.24199E+06 1 0.13233E-05 0.68259E+08 0.89967E+02 c temperature 0.00000E+00 0 0.00000E+00 0.13204E+03 0.92710E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.2107e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -216.08 216.08 0.0014225 0.00048622 v Velocity[Y] -0.13066 701.89 250.41 80.883 v Velocity[Z] -19.267 333.9 23.874 1.94 v ǁVelocityǁ 0.076051 701.9 259.25 83.628 v Pressure 55104 1.1026e+05 1.0384e+05 1.0417e+05 v k 1.2022e-08 40676 900.44 355.53 v omega 153.59 9.6772e+09 1.8448e+08 3.4138e+05 v TotEner 98800 6.2954e+05 3.415e+05 2.4849e+05 v temperature 72.53 533.99 398.28 337.15 v Density 0.42689 4.3268 0.95063 1.0905 v TurbVisc 8.9676e-19 0.064129 0.010064 0.028617 v CourantNb 1.2247e-05 40.9 0.36715 0.0075723 v FourierNb 4.5234e-05 238.89 1.9835 0.090492 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.598 533.99 403.78 422.09 v Boundary Density 0.42769 4.3265 0.98347 0.89717 v Yplus 0 42.742 2.4665 0.95136 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7131e-05 41.009 0.45385 0.010591 INSTANT 0.158693804E-01 TIME STEP NUMBER 30009 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.584576731E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561061671E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.126898067E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10407E+01 0.56741E+02 Friction velocity uk : 0.10407E+01 0.56741E+02 Dimensionless distance yplus : 0.20689E-01 0.42742E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14531E-01 0.12412E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60088E+03 7 0.83822E-07 0.65298E+03 0.61792E+03 c Velocity[X] 0.94427E+02 c Velocity[Y] 0.17084E+02 c Velocity[Z] 0.54147E+03 c Pressure 0.75301E-01 6 0.79193E-08 0.40539E+08 0.16757E+03 c k 0.24248E+04 1 0.97391E-06 0.23450E+06 0.24743E+04 c omega 0.81509E+09 1 0.96399E-08 0.66143E+13 0.18835E+03 c TotEner 0.24200E+06 1 0.13175E-05 0.57417E+08 0.82513E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10980E+03 0.84543E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1967e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -216.48 216.47 0.0014427 0.00049007 v Velocity[Y] -0.13066 701.89 250.41 80.884 v Velocity[Z] -19.266 333.92 23.907 1.9402 v ǁVelocityǁ 0.07585 701.9 259.27 83.629 v Pressure 55054 1.1026e+05 1.0383e+05 1.0417e+05 v k 1.2006e-08 40672 900.51 355.53 v omega 153.59 9.6772e+09 1.8448e+08 3.4138e+05 v TotEner 98752 6.2954e+05 3.415e+05 2.4849e+05 v temperature 72.465 533.99 398.27 337.15 v Density 0.42617 4.3272 0.95059 1.0905 v TurbVisc 8.9542e-19 0.064129 0.010065 0.028617 v CourantNb 1.2236e-05 40.951 0.36819 0.0075727 v FourierNb 4.5231e-05 241.13 1.9858 0.090493 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.53 533.99 403.81 422.09 v Boundary Density 0.42689 4.3268 0.98346 0.89718 v Yplus 0 42.742 2.4663 0.95139 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7145e-05 41.19 0.4552 0.010591 INSTANT 0.158696432E-01 TIME STEP NUMBER 30010 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.583088748E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561082128E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.126784345E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10404E+01 0.56781E+02 Friction velocity uk : 0.10404E+01 0.56781E+02 Dimensionless distance yplus : 0.20684E-01 0.42744E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14527E-01 0.12412E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60088E+03 7 0.80552E-07 0.62369E+03 0.60390E+03 c Velocity[X] 0.12456E+03 c Velocity[Y] 0.15837E+02 c Velocity[Z] 0.48330E+03 c Pressure 0.75305E-01 6 0.71899E-08 0.31920E+08 0.14869E+03 c k 0.24250E+04 1 0.97400E-06 0.28731E+06 0.27387E+04 c omega 0.81509E+09 1 0.86657E-08 0.51661E+13 0.16645E+03 c TotEner 0.24200E+06 1 0.13107E-05 0.46580E+08 0.74319E+02 c temperature 0.00000E+00 0 0.00000E+00 0.88031E+02 0.75700E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.185e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -216.79 216.78 0.0014606 0.00049393 v Velocity[Y] -0.13065 701.89 250.41 80.885 v Velocity[Z] -19.266 334.18 23.938 1.9404 v ǁVelocityǁ 0.075633 701.9 259.29 83.63 v Pressure 55011 1.1026e+05 1.0382e+05 1.0417e+05 v k 1.1993e-08 40664 900.58 355.53 v omega 153.6 9.6772e+09 1.8448e+08 3.4138e+05 v TotEner 98705 6.2954e+05 3.415e+05 2.4849e+05 v temperature 72.402 533.99 398.26 337.15 v Density 0.42554 4.3277 0.95055 1.0905 v TurbVisc 8.9427e-19 0.064129 0.010065 0.028617 v CourantNb 1.2227e-05 40.988 0.36907 0.007573 v FourierNb 4.5229e-05 243.47 1.9882 0.090495 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.465 533.99 403.83 422.09 v Boundary Density 0.42617 4.3272 0.98344 0.89718 v Yplus 0 42.744 2.466 0.95141 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7165e-05 41.341 0.45635 0.010591 INSTANT 0.158699060E-01 TIME STEP NUMBER 30011 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.581720627E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561098352E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.126675658E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10402E+01 0.56811E+02 Friction velocity uk : 0.10402E+01 0.56811E+02 Dimensionless distance yplus : 0.20678E-01 0.42747E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14523E-01 0.12412E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60089E+03 6 0.85863E-07 0.62085E+03 0.60252E+03 c Velocity[X] 0.18187E+03 c Velocity[Y] 0.14786E+02 c Velocity[Z] 0.42419E+03 c Pressure 0.75309E-01 6 0.64572E-08 0.23558E+08 0.12774E+03 c k 0.24251E+04 1 0.97584E-06 0.35354E+06 0.30378E+04 c omega 0.81509E+09 1 0.80350E-08 0.40878E+13 0.14807E+03 c TotEner 0.24200E+06 1 0.13036E-05 0.37445E+08 0.66634E+02 c temperature 0.00000E+00 0 0.00000E+00 0.69305E+02 0.67167E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1741e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -217.03 217.02 0.0014849 0.0004978 v Velocity[Y] -0.13065 701.89 250.41 80.886 v Velocity[Z] -19.265 334.58 23.966 1.9405 v ǁVelocityǁ 0.075401 701.9 259.31 83.631 v Pressure 54970 1.1026e+05 1.0382e+05 1.0417e+05 v k 1.1981e-08 40653 900.66 355.52 v omega 153.6 9.6772e+09 1.8448e+08 3.4138e+05 v TotEner 98660 6.2954e+05 3.4151e+05 2.4849e+05 v temperature 72.341 533.99 398.25 337.15 v Density 0.42498 4.3284 0.9505 1.0905 v TurbVisc 8.9327e-19 0.064129 0.010065 0.028617 v CourantNb 1.2219e-05 41.019 0.36986 0.0075732 v FourierNb 4.5226e-05 245.91 1.9879 0.090496 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.402 533.99 403.84 422.09 v Boundary Density 0.42554 4.3277 0.98342 0.89718 v Yplus 0 42.747 2.4656 0.95143 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7188e-05 41.482 0.45741 0.010592 INSTANT 0.158701688E-01 TIME STEP NUMBER 30012 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.580470181E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561110918E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.126572132E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10399E+01 0.56836E+02 Friction velocity uk : 0.10399E+01 0.56836E+02 Dimensionless distance yplus : 0.20674E-01 0.42750E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14520E-01 0.12412E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60089E+03 6 0.84691E-07 0.60383E+03 0.59420E+03 c Velocity[X] 0.22038E+03 c Velocity[Y] 0.14109E+02 c Velocity[Z] 0.36934E+03 c Pressure 0.75313E-01 6 0.61676E-08 0.17533E+08 0.11020E+03 c k 0.24253E+04 1 0.97922E-06 0.42872E+06 0.33451E+04 c omega 0.81509E+09 1 0.76529E-08 0.33665E+13 0.13437E+03 c TotEner 0.24200E+06 1 0.12972E-05 0.31802E+08 0.61408E+02 c temperature 0.00000E+00 0 0.00000E+00 0.57008E+02 0.60918E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1655e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -217.24 217.23 0.0015104 0.0005017 v Velocity[Y] -0.13064 701.89 250.41 80.887 v Velocity[Z] -19.265 335.1 23.991 1.9407 v ǁVelocityǁ 0.075154 701.9 259.33 83.632 v Pressure 54926 1.1026e+05 1.0381e+05 1.0417e+05 v k 1.1971e-08 40640 900.75 355.52 v omega 153.61 9.6772e+09 1.8448e+08 3.4138e+05 v TotEner 98617 6.2954e+05 3.4151e+05 2.4849e+05 v temperature 72.283 533.99 398.24 337.15 v Density 0.42446 4.3293 0.95047 1.0905 v TurbVisc 8.924e-19 0.064129 0.010065 0.028618 v CourantNb 1.2211e-05 41.048 0.37055 0.0075734 v FourierNb 4.5223e-05 247.61 1.9867 0.090497 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.341 533.99 403.85 422.09 v Boundary Density 0.42498 4.3284 0.9834 0.89718 v Yplus 0 42.75 2.465 0.95143 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.721e-05 41.595 0.4583 0.010592 INSTANT 0.158704317E-01 TIME STEP NUMBER 30013 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.579335186E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561120470E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.126473856E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10397E+01 0.56858E+02 Friction velocity uk : 0.10397E+01 0.56858E+02 Dimensionless distance yplus : 0.20670E-01 0.42754E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14517E-01 0.12412E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60089E+03 6 0.82287E-07 0.55289E+03 0.56858E+03 c Velocity[X] 0.22011E+03 c Velocity[Y] 0.13770E+02 c Velocity[Z] 0.31901E+03 c Pressure 0.75317E-01 6 0.56989E-08 0.14470E+08 0.10011E+03 c k 0.24255E+04 1 0.98350E-06 0.50588E+06 0.36335E+04 c omega 0.81509E+09 1 0.70945E-08 0.27869E+13 0.12226E+03 c TotEner 0.24200E+06 1 0.12914E-05 0.30161E+08 0.59803E+02 c temperature 0.00000E+00 0 0.00000E+00 0.51747E+02 0.58039E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1577e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -217.43 217.42 0.0015385 0.00050562 v Velocity[Y] -0.13064 701.89 250.41 80.888 v Velocity[Z] -19.264 335.68 24.015 1.9409 v ǁVelocityǁ 0.074892 701.9 259.35 83.633 v Pressure 54877 1.1026e+05 1.038e+05 1.0417e+05 v k 1.1962e-08 40627 900.86 355.52 v omega 153.61 9.6773e+09 1.8449e+08 3.4138e+05 v TotEner 98575 6.2954e+05 3.4151e+05 2.4849e+05 v temperature 72.226 533.99 398.23 337.15 v Density 0.42395 4.3303 0.95043 1.0905 v TurbVisc 8.9164e-19 0.064129 0.010065 0.028618 v CourantNb 1.2204e-05 41.078 0.37118 0.0075736 v FourierNb 4.522e-05 249.11 1.9839 0.090499 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.283 533.99 403.85 422.09 v Boundary Density 0.42446 4.3293 0.98337 0.89718 v Yplus 0 42.754 2.4644 0.95143 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7233e-05 41.698 0.45914 0.010592 INSTANT 0.158706945E-01 TIME STEP NUMBER 30014 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.578313388E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561127618E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.126380883E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10395E+01 0.56879E+02 Friction velocity uk : 0.10395E+01 0.56879E+02 Dimensionless distance yplus : 0.20666E-01 0.42758E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14514E-01 0.12412E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60089E+03 5 0.90433E-07 0.47191E+03 0.52528E+03 c Velocity[X] 0.18514E+03 c Velocity[Y] 0.13721E+02 c Velocity[Z] 0.27304E+03 c Pressure 0.75321E-01 6 0.75265E-08 0.13796E+08 0.97754E+02 c k 0.24257E+04 1 0.99071E-06 0.57472E+06 0.38725E+04 c omega 0.81509E+09 1 0.70143E-08 0.24541E+13 0.11472E+03 c TotEner 0.24200E+06 1 0.12860E-05 0.31636E+08 0.61247E+02 c temperature 0.00000E+00 0 0.00000E+00 0.51787E+02 0.58061E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1506e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -217.6 217.59 0.0015761 0.00050957 v Velocity[Y] -0.13063 701.89 250.41 80.889 v Velocity[Z] -19.264 336.26 24.036 1.941 v ǁVelocityǁ 0.074615 701.9 259.37 83.634 v Pressure 54818 1.1026e+05 1.038e+05 1.0417e+05 v k 1.1954e-08 40614 900.97 355.52 v omega 153.62 9.6773e+09 1.8449e+08 3.4139e+05 v TotEner 98534 6.2954e+05 3.4151e+05 2.4849e+05 v temperature 72.17 533.99 398.23 337.15 v Density 0.4234 4.3314 0.95039 1.0905 v TurbVisc 8.9097e-19 0.064129 0.010065 0.028618 v CourantNb 1.2197e-05 41.11 0.37176 0.0075738 v FourierNb 4.5218e-05 249.74 1.9786 0.0905 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.226 533.99 403.85 422.09 v Boundary Density 0.42395 4.3303 0.98334 0.89719 v Yplus 0 42.758 2.4636 0.9514 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7255e-05 41.792 0.45992 0.010593 INSTANT 0.158709574E-01 TIME STEP NUMBER 30015 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.577402497E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561132870E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.126293235E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10393E+01 0.56899E+02 Friction velocity uk : 0.10393E+01 0.56899E+02 Dimensionless distance yplus : 0.20662E-01 0.42764E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14512E-01 0.12413E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60089E+03 5 0.89110E-07 0.38361E+03 0.47360E+03 c Velocity[X] 0.13408E+03 c Velocity[Y] 0.13883E+02 c Velocity[Z] 0.23565E+03 c Pressure 0.75325E-01 6 0.64565E-08 0.14462E+08 0.10009E+03 c k 0.24259E+04 1 0.99834E-06 0.62806E+06 0.40480E+04 c omega 0.81509E+09 1 0.68535E-08 0.22471E+13 0.10978E+03 c TotEner 0.24200E+06 1 0.12812E-05 0.34505E+08 0.63964E+02 c temperature 0.00000E+00 0 0.00000E+00 0.54542E+02 0.59586E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1445e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -217.78 217.77 0.0016131 0.00051353 v Velocity[Y] -0.13063 701.89 250.41 80.89 v Velocity[Z] -19.263 336.79 24.056 1.9412 v ǁVelocityǁ 0.074324 701.9 259.38 83.635 v Pressure 54749 1.1026e+05 1.0379e+05 1.0417e+05 v k 1.1947e-08 40602 901.09 355.52 v omega 153.62 9.6773e+09 1.8449e+08 3.4139e+05 v TotEner 98494 6.2954e+05 3.4151e+05 2.4849e+05 v temperature 72.116 533.99 398.22 337.15 v Density 0.42282 4.3327 0.95035 1.0905 v TurbVisc 8.9038e-19 0.064129 0.010065 0.028618 v CourantNb 1.2192e-05 41.146 0.37227 0.007574 v FourierNb 4.5215e-05 249.36 1.9733 0.090501 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.17 533.99 403.84 422.09 v Boundary Density 0.4234 4.3314 0.9833 0.89719 v Yplus 0 42.764 2.4627 0.95136 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7277e-05 41.874 0.46057 0.010593 INSTANT 0.158712202E-01 TIME STEP NUMBER 30016 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.576600203E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561136636E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.126210903E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10392E+01 0.56920E+02 Friction velocity uk : 0.10392E+01 0.56920E+02 Dimensionless distance yplus : 0.20658E-01 0.42770E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14509E-01 0.12413E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60090E+03 5 0.85906E-07 0.30524E+03 0.42245E+03 c Velocity[X] 0.85550E+02 c Velocity[Y] 0.14078E+02 c Velocity[Z] 0.20561E+03 c Pressure 0.75329E-01 5 0.89386E-08 0.15317E+08 0.10300E+03 c k 0.24261E+04 1 0.10063E-05 0.66571E+06 0.41673E+04 c omega 0.81509E+09 1 0.67054E-08 0.21453E+13 0.10726E+03 c TotEner 0.24201E+06 1 0.12766E-05 0.36972E+08 0.66211E+02 c temperature 0.00000E+00 0 0.00000E+00 0.57010E+02 0.60918E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1384e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -217.96 217.95 0.0016471 0.00051748 v Velocity[Y] -0.13062 701.89 250.41 80.891 v Velocity[Z] -19.262 337.25 24.074 1.9414 v ǁVelocityǁ 0.07402 701.9 259.4 83.636 v Pressure 54668 1.1026e+05 1.0379e+05 1.0417e+05 v k 1.1941e-08 40592 901.21 355.52 v omega 153.63 9.6773e+09 1.8449e+08 3.4139e+05 v TotEner 98455 6.2954e+05 3.4151e+05 2.4849e+05 v temperature 72.064 533.99 398.21 337.15 v Density 0.42219 4.334 0.95032 1.0905 v TurbVisc 8.8985e-19 0.064129 0.010065 0.028618 v CourantNb 1.2187e-05 41.187 0.37276 0.0075742 v FourierNb 4.5212e-05 248.75 1.9679 0.090502 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.116 533.99 403.83 422.08 v Boundary Density 0.42282 4.3327 0.98325 0.89718 v Yplus 0 42.77 2.4617 0.95129 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7299e-05 41.954 0.4612 0.010593 INSTANT 0.158714831E-01 TIME STEP NUMBER 30017 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.575904146E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561139223E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.126133849E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10390E+01 0.56944E+02 Friction velocity uk : 0.10390E+01 0.56944E+02 Dimensionless distance yplus : 0.20655E-01 0.42776E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14507E-01 0.12413E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60090E+03 5 0.81217E-07 0.24865E+03 0.38128E+03 c Velocity[X] 0.52359E+02 c Velocity[Y] 0.14207E+02 c Velocity[Z] 0.18208E+03 c Pressure 0.75333E-01 5 0.90243E-08 0.15594E+08 0.10393E+03 c k 0.24264E+04 1 0.10129E-05 0.69303E+06 0.42516E+04 c omega 0.81509E+09 1 0.65390E-08 0.21529E+13 0.10745E+03 c TotEner 0.24201E+06 1 0.12722E-05 0.37716E+08 0.66874E+02 c temperature 0.00000E+00 0 0.00000E+00 0.57123E+02 0.60979E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1328e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -218.16 218.15 0.0016761 0.0005214 v Velocity[Y] -0.13062 701.89 250.42 80.892 v Velocity[Z] -19.262 337.64 24.092 1.9415 v ǁVelocityǁ 0.073703 701.9 259.41 83.637 v Pressure 54578 1.1026e+05 1.0378e+05 1.0417e+05 v k 1.1935e-08 40583 901.34 355.52 v omega 153.63 9.6773e+09 1.8449e+08 3.4139e+05 v TotEner 98417 6.2954e+05 3.4152e+05 2.4849e+05 v temperature 72.012 533.99 398.21 337.15 v Density 0.42151 4.3355 0.95029 1.0905 v TurbVisc 8.8938e-19 0.064129 0.010066 0.028619 v CourantNb 1.2183e-05 41.231 0.37322 0.0075744 v FourierNb 4.521e-05 247.49 1.9614 0.090503 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.064 533.99 403.82 422.08 v Boundary Density 0.42219 4.334 0.9832 0.89718 v Yplus 0 42.776 2.4606 0.95122 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.732e-05 42.029 0.46179 0.010593 INSTANT 0.158717460E-01 TIME STEP NUMBER 30018 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.575311956E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561140813E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.126062008E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10389E+01 0.56969E+02 Friction velocity uk : 0.10389E+01 0.56969E+02 Dimensionless distance yplus : 0.20652E-01 0.42783E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14505E-01 0.12414E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60090E+03 4 0.98341E-07 0.21485E+03 0.35442E+03 c Velocity[X] 0.37882E+02 c Velocity[Y] 0.14166E+02 c Velocity[Z] 0.16280E+03 c Pressure 0.75337E-01 6 0.63479E-08 0.14979E+08 0.10186E+03 c k 0.24266E+04 1 0.10182E-05 0.71766E+06 0.43263E+04 c omega 0.81509E+09 1 0.67037E-08 0.22832E+13 0.11066E+03 c TotEner 0.24201E+06 1 0.12676E-05 0.36211E+08 0.65526E+02 c temperature 0.00000E+00 0 0.00000E+00 0.54039E+02 0.59310E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1276e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -218.34 218.34 0.0017111 0.00052529 v Velocity[Y] -0.13061 701.89 250.42 80.893 v Velocity[Z] -19.261 337.96 24.108 1.9417 v ǁVelocityǁ 0.073372 701.9 259.43 83.637 v Pressure 54478 1.1026e+05 1.0378e+05 1.0417e+05 v k 1.193e-08 40575 901.47 355.52 v omega 153.64 9.6773e+09 1.8449e+08 3.4139e+05 v TotEner 98380 6.2954e+05 3.4152e+05 2.4849e+05 v temperature 71.961 533.99 398.2 337.15 v Density 0.42078 4.337 0.95026 1.0905 v TurbVisc 8.8896e-19 0.064129 0.010066 0.028619 v CourantNb 1.218e-05 41.278 0.37365 0.0075746 v FourierNb 4.5207e-05 245.52 1.954 0.090504 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 72.012 533.99 403.8 422.08 v Boundary Density 0.42151 4.3355 0.98314 0.89718 v Yplus 0 42.783 2.4594 0.95113 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7342e-05 42.099 0.46235 0.010594 INSTANT 0.158720088E-01 TIME STEP NUMBER 30019 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.574821233E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561141487E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125995287E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10387E+01 0.56996E+02 Friction velocity uk : 0.10387E+01 0.56996E+02 Dimensionless distance yplus : 0.20649E-01 0.42790E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14503E-01 0.12414E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60090E+03 4 0.95954E-07 0.20303E+03 0.34453E+03 c Velocity[X] 0.40494E+02 c Velocity[Y] 0.14052E+02 c Velocity[Z] 0.14849E+03 c Pressure 0.75341E-01 9 0.92406E-08 0.13621E+08 0.97132E+02 c k 0.24268E+04 1 0.10217E-05 0.74569E+06 0.44097E+04 c omega 0.81509E+09 1 0.70640E-08 0.25430E+13 0.11678E+03 c TotEner 0.24201E+06 1 0.12633E-05 0.32722E+08 0.62289E+02 c temperature 0.00000E+00 0 0.00000E+00 0.48413E+02 0.56137E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1237e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -218.55 218.55 0.0017369 0.00052912 v Velocity[Y] -0.13061 701.89 250.42 80.894 v Velocity[Z] -19.261 338.24 24.124 1.9418 v ǁVelocityǁ 0.07303 701.9 259.44 83.638 v Pressure 54374 1.1026e+05 1.0377e+05 1.0417e+05 v k 1.1926e-08 40568 901.59 355.52 v omega 153.64 9.6773e+09 1.8449e+08 3.4139e+05 v TotEner 98343 6.2954e+05 3.4152e+05 2.4849e+05 v temperature 71.911 533.99 398.2 337.15 v Density 0.42002 4.3386 0.95023 1.0905 v TurbVisc 8.8857e-19 0.064129 0.010066 0.028619 v CourantNb 1.2177e-05 41.326 0.37405 0.0075749 v FourierNb 4.5205e-05 243.25 1.9479 0.090505 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.961 533.99 403.78 422.08 v Boundary Density 0.42078 4.337 0.98309 0.89718 v Yplus 0 42.79 2.4583 0.95103 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7363e-05 42.152 0.46281 0.010594 INSTANT 0.158722717E-01 TIME STEP NUMBER 30020 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.574429540E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561141204E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125933567E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10386E+01 0.57024E+02 Friction velocity uk : 0.10386E+01 0.57024E+02 Dimensionless distance yplus : 0.20647E-01 0.42798E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14501E-01 0.12415E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60090E+03 4 0.92997E-07 0.20310E+03 0.34458E+03 c Velocity[X] 0.51871E+02 c Velocity[Y] 0.13865E+02 c Velocity[Z] 0.13736E+03 c Pressure 0.75345E-01 9 0.86730E-08 0.11883E+08 0.90726E+02 c k 0.24270E+04 1 0.10241E-05 0.77977E+06 0.45092E+04 c omega 0.81509E+09 1 0.69941E-08 0.27372E+13 0.12116E+03 c TotEner 0.24201E+06 1 0.12592E-05 0.28131E+08 0.57754E+02 c temperature 0.00000E+00 0 0.00000E+00 0.41551E+02 0.52007E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.12e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -218.77 218.77 0.001753 0.00053291 v Velocity[Y] -0.1306 701.89 250.42 80.895 v Velocity[Z] -19.26 338.5 24.139 1.942 v ǁVelocityǁ 0.072675 701.9 259.45 83.639 v Pressure 54266 1.1026e+05 1.0377e+05 1.0417e+05 v k 1.1921e-08 40561 901.71 355.52 v omega 153.65 9.6773e+09 1.845e+08 3.4139e+05 v TotEner 98307 6.2954e+05 3.4152e+05 2.4849e+05 v temperature 71.862 533.99 398.19 337.15 v Density 0.41925 4.3403 0.9502 1.0905 v TurbVisc 8.8823e-19 0.064129 0.010066 0.028619 v CourantNb 1.2175e-05 41.376 0.37443 0.0075751 v FourierNb 4.5202e-05 241.15 1.9427 0.090506 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.911 533.99 403.76 422.07 v Boundary Density 0.42002 4.3386 0.98303 0.89717 v Yplus 0 42.798 2.4572 0.95094 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7384e-05 42.202 0.46326 0.010594 INSTANT 0.158725346E-01 TIME STEP NUMBER 30021 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.574134427E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561139967E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125876703E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10384E+01 0.57053E+02 Friction velocity uk : 0.10384E+01 0.57053E+02 Dimensionless distance yplus : 0.20644E-01 0.42806E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14499E-01 0.12415E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60090E+03 4 0.89644E-07 0.20556E+03 0.34666E+03 c Velocity[X] 0.63407E+02 c Velocity[Y] 0.13642E+02 c Velocity[Z] 0.12851E+03 c Pressure 0.75349E-01 9 0.81163E-08 0.10205E+08 0.84073E+02 c k 0.24271E+04 1 0.10258E-05 0.81918E+06 0.46216E+04 c omega 0.81509E+09 1 0.73688E-08 0.30723E+13 0.12836E+03 c TotEner 0.24201E+06 1 0.12552E-05 0.23468E+08 0.52751E+02 c temperature 0.00000E+00 0 0.00000E+00 0.35024E+02 0.47748E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1164e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -219 219 0.0017598 0.00053664 v Velocity[Y] -0.1306 701.89 250.42 80.896 v Velocity[Z] -19.259 338.75 24.154 1.9422 v ǁVelocityǁ 0.07231 701.9 259.47 83.64 v Pressure 54156 1.1026e+05 1.0376e+05 1.0417e+05 v k 1.1917e-08 40555 901.83 355.52 v omega 153.65 9.6773e+09 1.845e+08 3.4139e+05 v TotEner 98271 6.2954e+05 3.4152e+05 2.4849e+05 v temperature 71.813 533.99 398.18 337.15 v Density 0.41847 4.342 0.95017 1.0905 v TurbVisc 8.8791e-19 0.064129 0.010066 0.028619 v CourantNb 1.2174e-05 41.425 0.3748 0.0075754 v FourierNb 4.5199e-05 239.01 1.9376 0.090507 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.862 533.99 403.74 422.07 v Boundary Density 0.41925 4.3403 0.98298 0.89717 v Yplus 0 42.806 2.4561 0.95086 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7404e-05 42.25 0.4637 0.010595 INSTANT 0.158727975E-01 TIME STEP NUMBER 30022 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.573933438E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561137667E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125824519E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10383E+01 0.57083E+02 Friction velocity uk : 0.10383E+01 0.57083E+02 Dimensionless distance yplus : 0.20641E-01 0.42815E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14497E-01 0.12416E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60091E+03 4 0.86232E-07 0.20356E+03 0.34497E+03 c Velocity[X] 0.68872E+02 c Velocity[Y] 0.13420E+02 c Velocity[Z] 0.12126E+03 c Pressure 0.75353E-01 9 0.76895E-08 0.89120E+07 0.78569E+02 c k 0.24273E+04 1 0.10268E-05 0.86163E+06 0.47396E+04 c omega 0.81509E+09 1 0.76742E-08 0.33254E+13 0.13355E+03 c TotEner 0.24201E+06 1 0.12515E-05 0.19549E+08 0.48146E+02 c temperature 0.00000E+00 0 0.00000E+00 0.29996E+02 0.44187E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1131e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -219.23 219.23 0.0017586 0.00054034 v Velocity[Y] -0.13059 701.89 250.42 80.897 v Velocity[Z] -19.259 339.01 24.168 1.9423 v ǁVelocityǁ 0.071934 701.9 259.48 83.641 v Pressure 54048 1.1026e+05 1.0376e+05 1.0417e+05 v k 1.1914e-08 40552 901.95 355.51 v omega 153.65 9.6774e+09 1.845e+08 3.4139e+05 v TotEner 98236 6.2954e+05 3.4152e+05 2.4849e+05 v temperature 71.765 533.99 398.18 337.15 v Density 0.4177 4.3439 0.95014 1.0905 v TurbVisc 8.876e-19 0.064129 0.010066 0.028619 v CourantNb 1.2174e-05 41.474 0.37515 0.0075757 v FourierNb 4.5197e-05 236.79 1.9324 0.090508 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.813 533.99 403.72 422.07 v Boundary Density 0.41847 4.342 0.98294 0.89717 v Yplus 0 42.815 2.4552 0.95079 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7425e-05 42.296 0.46412 0.010595 INSTANT 0.158730604E-01 TIME STEP NUMBER 30023 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.573824084E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561134157E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125776814E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10382E+01 0.57114E+02 Friction velocity uk : 0.10382E+01 0.57114E+02 Dimensionless distance yplus : 0.20639E-01 0.42823E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14496E-01 0.12416E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60091E+03 3 0.13947E-06 0.19289E+03 0.33580E+03 c Velocity[X] 0.65314E+02 c Velocity[Y] 0.13136E+02 c Velocity[Z] 0.11444E+03 c Pressure 0.75357E-01 9 0.72998E-08 0.81197E+07 0.74995E+02 c k 0.24274E+04 1 0.10274E-05 0.90477E+06 0.48566E+04 c omega 0.81509E+09 1 0.77582E-08 0.35741E+13 0.13845E+03 c TotEner 0.24202E+06 1 0.12477E-05 0.16769E+08 0.44590E+02 c temperature 0.00000E+00 0 0.00000E+00 0.26831E+02 0.41792E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1099e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -219.42 219.42 0.0017725 0.000544 v Velocity[Y] -0.13059 701.89 250.43 80.898 v Velocity[Z] -19.258 339.28 24.182 1.9425 v ǁVelocityǁ 0.071548 701.9 259.49 83.642 v Pressure 53942 1.1026e+05 1.0375e+05 1.0417e+05 v k 1.191e-08 40551 902.07 355.51 v omega 153.66 9.6774e+09 1.845e+08 3.4139e+05 v TotEner 98201 6.2954e+05 3.4152e+05 2.4849e+05 v temperature 71.717 533.99 398.17 337.15 v Density 0.41694 4.3457 0.95011 1.0905 v TurbVisc 8.8731e-19 0.064129 0.010066 0.02862 v CourantNb 1.2174e-05 41.521 0.37549 0.0075759 v FourierNb 4.5194e-05 234.55 1.9274 0.090509 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.765 533.99 403.71 422.07 v Boundary Density 0.4177 4.3439 0.98291 0.89717 v Yplus 0 42.823 2.4545 0.95074 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7445e-05 42.339 0.46452 0.010595 INSTANT 0.158733232E-01 TIME STEP NUMBER 30024 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.573803858E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561129299E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125733357E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10381E+01 0.57143E+02 Friction velocity uk : 0.10381E+01 0.57143E+02 Dimensionless distance yplus : 0.20637E-01 0.42832E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14494E-01 0.12417E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60091E+03 3 0.13853E-06 0.17726E+03 0.32191E+03 c Velocity[X] 0.55353E+02 c Velocity[Y] 0.12931E+02 c Velocity[Z] 0.10898E+03 c Pressure 0.75361E-01 9 0.73294E-08 0.77925E+07 0.73468E+02 c k 0.24275E+04 1 0.10251E-05 0.95095E+06 0.49789E+04 c omega 0.81509E+09 1 0.79523E-08 0.38411E+13 0.14353E+03 c TotEner 0.24202E+06 1 0.12445E-05 0.15039E+08 0.42228E+02 c temperature 0.00000E+00 0 0.00000E+00 0.25410E+02 0.40670E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1075e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -219.63 219.64 0.0017797 0.00054764 v Velocity[Y] -0.13059 701.89 250.43 80.898 v Velocity[Z] -19.258 339.57 24.195 1.9427 v ǁVelocityǁ 0.071153 701.9 259.5 83.643 v Pressure 53841 1.1026e+05 1.0375e+05 1.0417e+05 v k 1.1906e-08 40555 902.19 355.51 v omega 153.66 9.6774e+09 1.845e+08 3.4139e+05 v TotEner 98166 6.2954e+05 3.4152e+05 2.4849e+05 v temperature 71.669 533.99 398.17 337.15 v Density 0.41622 4.3476 0.95009 1.0905 v TurbVisc 8.8704e-19 0.064129 0.010067 0.02862 v CourantNb 1.2176e-05 41.565 0.3758 0.0075762 v FourierNb 4.5192e-05 232.59 1.9237 0.090511 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.717 533.99 403.7 422.06 v Boundary Density 0.41694 4.3457 0.98289 0.89717 v Yplus 0 42.832 2.4538 0.95071 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7466e-05 42.371 0.46485 0.010596 INSTANT 0.158735861E-01 TIME STEP NUMBER 30025 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.573870238E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561122987E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125693902E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10380E+01 0.57171E+02 Friction velocity uk : 0.10380E+01 0.57171E+02 Dimensionless distance yplus : 0.20635E-01 0.42842E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14493E-01 0.12417E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60091E+03 3 0.13743E-06 0.15901E+03 0.30489E+03 c Velocity[X] 0.41992E+02 c Velocity[Y] 0.12789E+02 c Velocity[Z] 0.10423E+03 c Pressure 0.75365E-01 6 0.95005E-08 0.77416E+07 0.73228E+02 c k 0.24276E+04 1 0.10238E-05 0.99273E+06 0.50868E+04 c omega 0.81509E+09 1 0.76842E-08 0.38274E+13 0.14327E+03 c TotEner 0.24202E+06 1 0.12416E-05 0.14123E+08 0.40922E+02 c temperature 0.00000E+00 0 0.00000E+00 0.25029E+02 0.40364E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1052e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -219.84 219.85 0.0017809 0.00055128 v Velocity[Y] -0.13058 701.89 250.43 80.899 v Velocity[Z] -19.257 339.89 24.208 1.9428 v ǁVelocityǁ 0.070749 701.9 259.51 83.644 v Pressure 53747 1.1026e+05 1.0375e+05 1.0417e+05 v k 1.1903e-08 40563 902.32 355.51 v omega 153.67 9.6774e+09 1.8451e+08 3.4139e+05 v TotEner 98132 6.2954e+05 3.4152e+05 2.4849e+05 v temperature 71.622 533.99 398.16 337.15 v Density 0.41554 4.3496 0.95006 1.0905 v TurbVisc 8.8677e-19 0.064129 0.010067 0.02862 v CourantNb 1.2177e-05 41.607 0.3761 0.0075765 v FourierNb 4.519e-05 230.99 1.921 0.090512 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.669 533.99 403.68 422.06 v Boundary Density 0.41622 4.3476 0.98287 0.89717 v Yplus 0 42.842 2.4533 0.95069 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7486e-05 42.402 0.46517 0.010596 INSTANT 0.158738490E-01 TIME STEP NUMBER 30026 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.574020687E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561115151E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125658141E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10379E+01 0.57199E+02 Friction velocity uk : 0.10379E+01 0.57199E+02 Dimensionless distance yplus : 0.20633E-01 0.42851E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14491E-01 0.12418E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60091E+03 3 0.13617E-06 0.14172E+03 0.28783E+03 c Velocity[X] 0.29067E+02 c Velocity[Y] 0.12665E+02 c Velocity[Z] 0.99983E+02 c Pressure 0.75369E-01 6 0.95770E-08 0.77602E+07 0.73316E+02 c k 0.24278E+04 1 0.10222E-05 0.10293E+07 0.51794E+04 c omega 0.81509E+09 1 0.75423E-08 0.38278E+13 0.14328E+03 c TotEner 0.24202E+06 1 0.12389E-05 0.13632E+08 0.40204E+02 c temperature 0.00000E+00 0 0.00000E+00 0.24964E+02 0.40311E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.103e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -220.04 220.05 0.001777 0.00055493 v Velocity[Y] -0.13058 701.89 250.43 80.9 v Velocity[Z] -19.256 340.22 24.22 1.943 v ǁVelocityǁ 0.070081 701.9 259.52 83.645 v Pressure 53658 1.1026e+05 1.0374e+05 1.0417e+05 v k 1.1899e-08 40576 902.46 355.51 v omega 153.67 9.6774e+09 1.8451e+08 3.414e+05 v TotEner 98097 6.2954e+05 3.4153e+05 2.4849e+05 v temperature 71.575 533.99 398.16 337.15 v Density 0.41491 4.3516 0.95004 1.0905 v TurbVisc 8.8651e-19 0.064129 0.010067 0.02862 v CourantNb 1.218e-05 41.645 0.37639 0.0075767 v FourierNb 4.5187e-05 229.62 1.9186 0.090514 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.622 533.99 403.67 422.06 v Boundary Density 0.41554 4.3496 0.98286 0.89717 v Yplus 0 42.851 2.4528 0.95069 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7506e-05 42.434 0.46549 0.010596 INSTANT 0.158741119E-01 TIME STEP NUMBER 30027 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.574252659E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561105798E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125625749E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10378E+01 0.57225E+02 Friction velocity uk : 0.10378E+01 0.57225E+02 Dimensionless distance yplus : 0.20631E-01 0.42861E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14490E-01 0.12418E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60092E+03 3 0.13489E-06 0.12797E+03 0.27351E+03 c Velocity[X] 0.19377E+02 c Velocity[Y] 0.12550E+02 c Velocity[Z] 0.96042E+02 c Pressure 0.75373E-01 6 0.96461E-08 0.76914E+07 0.72990E+02 c k 0.24280E+04 1 0.10196E-05 0.10593E+07 0.52541E+04 c omega 0.81510E+09 1 0.78529E-08 0.38630E+13 0.14393E+03 c TotEner 0.24202E+06 1 0.12363E-05 0.13272E+08 0.39670E+02 c temperature 0.00000E+00 0 0.00000E+00 0.24696E+02 0.40094E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.1007e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -220.23 220.25 0.0017689 0.00055857 v Velocity[Y] -0.13057 701.89 250.43 80.901 v Velocity[Z] -19.256 340.57 24.233 1.9432 v ǁVelocityǁ 0.069285 701.9 259.54 83.646 v Pressure 53576 1.1026e+05 1.0374e+05 1.0417e+05 v k 1.1896e-08 40593 902.6 355.51 v omega 153.68 9.6774e+09 1.8451e+08 3.414e+05 v TotEner 98063 6.2954e+05 3.4153e+05 2.4849e+05 v temperature 71.528 533.99 398.15 337.15 v Density 0.41431 4.3536 0.95001 1.0905 v TurbVisc 8.8626e-19 0.064129 0.010067 0.02862 v CourantNb 1.2183e-05 41.682 0.37667 0.0075769 v FourierNb 4.5185e-05 228.42 1.9164 0.090515 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.575 533.99 403.66 422.06 v Boundary Density 0.41491 4.3516 0.98286 0.89718 v Yplus 0 42.861 2.4525 0.9507 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7526e-05 42.465 0.4658 0.010597 INSTANT 0.158743748E-01 TIME STEP NUMBER 30028 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.574563592E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561094926E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125596368E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10377E+01 0.57249E+02 Friction velocity uk : 0.10377E+01 0.57249E+02 Dimensionless distance yplus : 0.20630E-01 0.42871E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14489E-01 0.12419E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60092E+03 3 0.13370E-06 0.11869E+03 0.26341E+03 c Velocity[X] 0.14021E+02 c Velocity[Y] 0.12397E+02 c Velocity[Z] 0.92276E+02 c Pressure 0.75377E-01 6 0.93276E-08 0.74658E+07 0.71912E+02 c k 0.24282E+04 1 0.10142E-05 0.10808E+07 0.53068E+04 c omega 0.81510E+09 1 0.80291E-08 0.38871E+13 0.14438E+03 c TotEner 0.24202E+06 1 0.12337E-05 0.12889E+08 0.39092E+02 c temperature 0.00000E+00 0 0.00000E+00 0.24018E+02 0.39540E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0984e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -220.42 220.43 0.0017574 0.00056223 v Velocity[Y] -0.13057 701.89 250.43 80.902 v Velocity[Z] -19.255 340.94 24.245 1.9433 v ǁVelocityǁ 0.068462 701.9 259.55 83.647 v Pressure 53499 1.1026e+05 1.0373e+05 1.0417e+05 v k 1.1893e-08 40612 902.76 355.51 v omega 153.68 9.6774e+09 1.8451e+08 3.414e+05 v TotEner 98029 6.2954e+05 3.4153e+05 2.4849e+05 v temperature 71.482 533.99 398.15 337.15 v Density 0.41375 4.3557 0.94999 1.0905 v TurbVisc 8.8602e-19 0.064129 0.010067 0.028621 v CourantNb 1.2187e-05 41.716 0.37695 0.0075771 v FourierNb 4.5182e-05 227.35 1.9143 0.090517 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.528 533.99 403.65 422.06 v Boundary Density 0.41431 4.3536 0.98286 0.89718 v Yplus 0 42.871 2.4522 0.95072 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7546e-05 42.496 0.4661 0.010597 INSTANT 0.158746377E-01 TIME STEP NUMBER 30029 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.574950915E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561082614E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125569610E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10376E+01 0.57273E+02 Friction velocity uk : 0.10376E+01 0.57273E+02 Dimensionless distance yplus : 0.20628E-01 0.42881E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14488E-01 0.12419E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60092E+03 3 0.13268E-06 0.11337E+03 0.25743E+03 c Velocity[X] 0.12505E+02 c Velocity[Y] 0.12267E+02 c Velocity[Z] 0.88596E+02 c Pressure 0.75381E-01 6 0.81796E-08 0.70995E+07 0.70126E+02 c k 0.24284E+04 1 0.10092E-05 0.10918E+07 0.53334E+04 c omega 0.81510E+09 1 0.77730E-08 0.37274E+13 0.14139E+03 c TotEner 0.24202E+06 1 0.12312E-05 0.12494E+08 0.38489E+02 c temperature 0.00000E+00 0 0.00000E+00 0.23016E+02 0.38707E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0962e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -220.6 220.61 0.0017431 0.00056588 v Velocity[Y] -0.13056 701.89 250.43 80.903 v Velocity[Z] -19.255 341.31 24.257 1.9435 v ǁVelocityǁ 0.067615 701.9 259.56 83.647 v Pressure 53428 1.1026e+05 1.0373e+05 1.0417e+05 v k 1.189e-08 40633 902.92 355.51 v omega 153.69 9.6775e+09 1.8452e+08 3.414e+05 v TotEner 97995 6.2954e+05 3.4153e+05 2.4849e+05 v temperature 71.435 533.99 398.15 337.15 v Density 0.41323 4.3579 0.94997 1.0905 v TurbVisc 8.8579e-19 0.064129 0.010068 0.028621 v CourantNb 1.2192e-05 41.749 0.37721 0.0075773 v FourierNb 4.518e-05 226.39 1.9121 0.090518 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.482 533.99 403.65 422.06 v Boundary Density 0.41375 4.3557 0.98287 0.89719 v Yplus 0 42.881 2.4519 0.95075 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7566e-05 42.526 0.4664 0.010597 INSTANT 0.158749006E-01 TIME STEP NUMBER 30030 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.575412051E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561068984E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125545052E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10376E+01 0.57295E+02 Friction velocity uk : 0.10376E+01 0.57295E+02 Dimensionless distance yplus : 0.20626E-01 0.42891E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14486E-01 0.12420E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60092E+03 3 0.13182E-06 0.11046E+03 0.25410E+03 c Velocity[X] 0.13350E+02 c Velocity[Y] 0.12151E+02 c Velocity[Z] 0.84961E+02 c Pressure 0.75385E-01 6 0.79729E-08 0.66635E+07 0.67938E+02 c k 0.24287E+04 1 0.10046E-05 0.10910E+07 0.53308E+04 c omega 0.81510E+09 1 0.76443E-08 0.35680E+13 0.13833E+03 c TotEner 0.24203E+06 1 0.12288E-05 0.12157E+08 0.37966E+02 c temperature 0.00000E+00 0 0.00000E+00 0.21927E+02 0.37780E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.094e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -220.76 220.77 0.0017267 0.00056953 v Velocity[Y] -0.13056 701.89 250.44 80.904 v Velocity[Z] -19.254 341.68 24.268 1.9437 v ǁVelocityǁ 0.066741 701.9 259.57 83.648 v Pressure 53361 1.1026e+05 1.0373e+05 1.0417e+05 v k 1.1888e-08 40654 903.08 355.51 v omega 153.69 9.6775e+09 1.8452e+08 3.414e+05 v TotEner 97961 6.2954e+05 3.4153e+05 2.4849e+05 v temperature 71.388 533.99 398.14 337.15 v Density 0.41275 4.36 0.94995 1.0905 v TurbVisc 8.8558e-19 0.064129 0.010068 0.028621 v CourantNb 1.2198e-05 41.78 0.37747 0.0075775 v FourierNb 4.5178e-05 225.53 1.9101 0.09052 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.435 533.99 403.64 422.06 v Boundary Density 0.41323 4.3579 0.98288 0.89719 v Yplus 0 42.891 2.4517 0.95078 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7586e-05 42.556 0.46668 0.010598 INSTANT 0.158751635E-01 TIME STEP NUMBER 30031 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.575944419E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561054202E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125522240E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10375E+01 0.57316E+02 Friction velocity uk : 0.10375E+01 0.57316E+02 Dimensionless distance yplus : 0.20624E-01 0.42902E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14485E-01 0.12420E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60092E+03 3 0.13108E-06 0.10831E+03 0.25161E+03 c Velocity[X] 0.14868E+02 c Velocity[Y] 0.12069E+02 c Velocity[Z] 0.81374E+02 c Pressure 0.75389E-01 6 0.76845E-08 0.62436E+07 0.65763E+02 c k 0.24289E+04 1 0.10005E-05 0.10777E+07 0.52979E+04 c omega 0.81510E+09 1 0.75908E-08 0.34577E+13 0.13617E+03 c TotEner 0.24203E+06 1 0.12266E-05 0.11961E+08 0.37659E+02 c temperature 0.00000E+00 0 0.00000E+00 0.21003E+02 0.36975E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0918e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -220.92 220.93 0.0017091 0.00057319 v Velocity[Y] -0.13055 701.89 250.44 80.905 v Velocity[Z] -19.254 342.06 24.28 1.9438 v ǁVelocityǁ 0.065843 701.9 259.57 83.649 v Pressure 53299 1.1026e+05 1.0372e+05 1.0417e+05 v k 1.1885e-08 40673 903.25 355.51 v omega 153.7 9.6775e+09 1.8452e+08 3.414e+05 v TotEner 97927 6.2954e+05 3.4153e+05 2.4849e+05 v temperature 71.341 533.99 398.14 337.15 v Density 0.41229 4.3622 0.94993 1.0905 v TurbVisc 8.8537e-19 0.064129 0.010068 0.028621 v CourantNb 1.2204e-05 41.809 0.37772 0.0075777 v FourierNb 4.5175e-05 224.76 1.9081 0.090522 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.388 533.99 403.63 422.06 v Boundary Density 0.41275 4.36 0.98289 0.8972 v Yplus 0 42.902 2.4514 0.9508 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7606e-05 42.586 0.46696 0.010598 INSTANT 0.158754264E-01 TIME STEP NUMBER 30032 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.576545431E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561038444E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125500693E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10374E+01 0.57335E+02 Friction velocity uk : 0.10374E+01 0.57335E+02 Dimensionless distance yplus : 0.20623E-01 0.42913E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14484E-01 0.12421E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60093E+03 3 0.13042E-06 0.10562E+03 0.24846E+03 c Velocity[X] 0.15769E+02 c Velocity[Y] 0.11974E+02 c Velocity[Z] 0.77874E+02 c Pressure 0.75393E-01 6 0.75265E-08 0.59047E+07 0.63953E+02 c k 0.24292E+04 1 0.99478E-06 0.10525E+07 0.52352E+04 c omega 0.81510E+09 1 0.74268E-08 0.32701E+13 0.13243E+03 c TotEner 0.24203E+06 1 0.12244E-05 0.11926E+08 0.37605E+02 c temperature 0.00000E+00 0 0.00000E+00 0.20392E+02 0.36433E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0897e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -221.07 221.08 0.0016906 0.00057687 v Velocity[Y] -0.13055 701.89 250.44 80.906 v Velocity[Z] -19.253 342.44 24.291 1.944 v ǁVelocityǁ 0.064919 701.9 259.58 83.65 v Pressure 53241 1.1026e+05 1.0372e+05 1.0417e+05 v k 1.1883e-08 40689 903.43 355.51 v omega 153.7 9.6775e+09 1.8452e+08 3.414e+05 v TotEner 97893 6.2954e+05 3.4153e+05 2.4849e+05 v temperature 71.294 533.99 398.13 337.16 v Density 0.41187 4.3644 0.94991 1.0905 v TurbVisc 8.8517e-19 0.064129 0.010068 0.028621 v CourantNb 1.2211e-05 41.838 0.37797 0.0075779 v FourierNb 4.5173e-05 224.08 1.9062 0.090523 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.341 533.99 403.62 422.05 v Boundary Density 0.41229 4.3622 0.9829 0.89721 v Yplus 0 42.913 2.4512 0.95083 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7626e-05 42.616 0.46724 0.010598 INSTANT 0.158756894E-01 TIME STEP NUMBER 30033 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.577212498E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561021917E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125479905E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10373E+01 0.57353E+02 Friction velocity uk : 0.10373E+01 0.57353E+02 Dimensionless distance yplus : 0.20621E-01 0.42923E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14483E-01 0.12422E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60093E+03 3 0.12979E-06 0.10192E+03 0.24407E+03 c Velocity[X] 0.15473E+02 c Velocity[Y] 0.11918E+02 c Velocity[Z] 0.74524E+02 c Pressure 0.75397E-01 5 0.93798E-08 0.56726E+07 0.62683E+02 c k 0.24295E+04 1 0.98950E-06 0.10169E+07 0.51454E+04 c omega 0.81510E+09 1 0.72550E-08 0.30755E+13 0.12843E+03 c TotEner 0.24203E+06 1 0.12224E-05 0.12031E+08 0.37769E+02 c temperature 0.00000E+00 0 0.00000E+00 0.20112E+02 0.36182E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0876e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -221.2 221.22 0.0016719 0.00058056 v Velocity[Y] -0.13054 701.89 250.44 80.907 v Velocity[Z] -19.252 342.8 24.302 1.9442 v ǁVelocityǁ 0.06397 701.9 259.59 83.651 v Pressure 53186 1.1026e+05 1.0372e+05 1.0417e+05 v k 1.188e-08 40701 903.6 355.51 v omega 153.71 9.6775e+09 1.8453e+08 3.414e+05 v TotEner 97859 6.2953e+05 3.4153e+05 2.485e+05 v temperature 71.247 533.98 398.13 337.16 v Density 0.41147 4.3667 0.94989 1.0905 v TurbVisc 8.8499e-19 0.064129 0.010068 0.028622 v CourantNb 1.2219e-05 41.865 0.37821 0.007578 v FourierNb 4.5171e-05 223.49 1.9045 0.090525 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.294 533.99 403.61 422.05 v Boundary Density 0.41187 4.3644 0.9829 0.89721 v Yplus 0 42.923 2.4509 0.95084 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7646e-05 42.645 0.4675 0.010598 INSTANT 0.158759523E-01 TIME STEP NUMBER 30034 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.577943031E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561004835E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125459347E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10372E+01 0.57370E+02 Friction velocity uk : 0.10372E+01 0.57370E+02 Dimensionless distance yplus : 0.20620E-01 0.42934E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14482E-01 0.12422E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60093E+03 3 0.12918E-06 0.97358E+02 0.23855E+03 c Velocity[X] 0.14081E+02 c Velocity[Y] 0.11881E+02 c Velocity[Z] 0.71396E+02 c Pressure 0.75401E-01 5 0.89173E-08 0.55360E+07 0.61925E+02 c k 0.24298E+04 1 0.98405E-06 0.97257E+06 0.50316E+04 c omega 0.81510E+09 1 0.71540E-08 0.28614E+13 0.12388E+03 c TotEner 0.24203E+06 1 0.12205E-05 0.12187E+08 0.38013E+02 c temperature 0.00000E+00 0 0.00000E+00 0.20059E+02 0.36135E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0855e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -221.33 221.35 0.0016536 0.00058425 v Velocity[Y] -0.13054 701.89 250.44 80.908 v Velocity[Z] -19.252 343.16 24.313 1.9443 v ǁVelocityǁ 0.062997 701.9 259.6 83.652 v Pressure 53134 1.1026e+05 1.0371e+05 1.0417e+05 v k 1.1878e-08 40709 903.78 355.5 v omega 153.71 9.6775e+09 1.8453e+08 3.414e+05 v TotEner 97824 6.2953e+05 3.4153e+05 2.485e+05 v temperature 71.2 533.98 398.13 337.16 v Density 0.41108 4.3689 0.94987 1.0905 v TurbVisc 8.848e-19 0.064129 0.010069 0.028622 v CourantNb 1.2227e-05 41.891 0.37844 0.0075782 v FourierNb 4.5169e-05 222.96 1.9028 0.090526 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.247 533.98 403.6 422.05 v Boundary Density 0.41147 4.3667 0.98291 0.89721 v Yplus 0 42.934 2.4507 0.95085 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7665e-05 42.674 0.46776 0.010599 INSTANT 0.158762152E-01 TIME STEP NUMBER 30035 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.578734448E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560987408E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125438476E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10372E+01 0.57386E+02 Friction velocity uk : 0.10372E+01 0.57386E+02 Dimensionless distance yplus : 0.20618E-01 0.42945E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14481E-01 0.12423E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60093E+03 3 0.12857E-06 0.92521E+02 0.23254E+03 c Velocity[X] 0.12126E+02 c Velocity[Y] 0.11846E+02 c Velocity[Z] 0.68548E+02 c Pressure 0.75405E-01 5 0.96273E-08 0.54578E+07 0.61486E+02 c k 0.24301E+04 1 0.97772E-06 0.92154E+06 0.48974E+04 c omega 0.81510E+09 1 0.70277E-08 0.26726E+13 0.11972E+03 c TotEner 0.24203E+06 1 0.12187E-05 0.12289E+08 0.38171E+02 c temperature 0.00000E+00 0 0.00000E+00 0.20069E+02 0.36144E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0835e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -221.46 221.47 0.001636 0.00058795 v Velocity[Y] -0.13053 701.89 250.44 80.909 v Velocity[Z] -19.251 343.52 24.324 1.9445 v ǁVelocityǁ 0.061998 701.9 259.61 83.653 v Pressure 53084 1.1026e+05 1.0371e+05 1.0417e+05 v k 1.1876e-08 40713 903.95 355.5 v omega 153.72 9.6775e+09 1.8453e+08 3.414e+05 v TotEner 97789 6.2953e+05 3.4153e+05 2.485e+05 v temperature 71.152 533.98 398.12 337.16 v Density 0.41072 4.3712 0.94985 1.0905 v TurbVisc 8.8462e-19 0.064129 0.010069 0.028622 v CourantNb 1.2236e-05 41.917 0.37867 0.0075784 v FourierNb 4.5166e-05 222.5 1.9012 0.090528 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.2 533.98 403.58 422.05 v Boundary Density 0.41108 4.3689 0.98292 0.89722 v Yplus 0 42.945 2.4504 0.95086 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7685e-05 42.702 0.46802 0.010599 INSTANT 0.158764781E-01 TIME STEP NUMBER 30036 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.579584157E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560969841E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125416738E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10371E+01 0.57401E+02 Friction velocity uk : 0.10371E+01 0.57401E+02 Dimensionless distance yplus : 0.20617E-01 0.42956E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14480E-01 0.12423E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60093E+03 3 0.12797E-06 0.88093E+02 0.22691E+03 c Velocity[X] 0.10248E+02 c Velocity[Y] 0.11822E+02 c Velocity[Z] 0.66023E+02 c Pressure 0.75409E-01 5 0.96587E-08 0.53943E+07 0.61127E+02 c k 0.24304E+04 1 0.97113E-06 0.86583E+06 0.47467E+04 c omega 0.81510E+09 1 0.71421E-08 0.25146E+13 0.11613E+03 c TotEner 0.24203E+06 1 0.12170E-05 0.12253E+08 0.38116E+02 c temperature 0.00000E+00 0 0.00000E+00 0.19988E+02 0.36070E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0815e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -221.58 221.59 0.0016195 0.00059166 v Velocity[Y] -0.13053 701.89 250.44 80.91 v Velocity[Z] -19.251 343.86 24.334 1.9447 v ǁVelocityǁ 0.060975 701.9 259.62 83.654 v Pressure 53036 1.1026e+05 1.0371e+05 1.0417e+05 v k 1.1873e-08 40714 904.12 355.5 v omega 153.72 9.6775e+09 1.8453e+08 3.414e+05 v TotEner 97754 6.2953e+05 3.4153e+05 2.485e+05 v temperature 71.104 533.98 398.12 337.16 v Density 0.41036 4.3735 0.94983 1.0905 v TurbVisc 8.8445e-19 0.064129 0.010069 0.028622 v CourantNb 1.2246e-05 41.942 0.37889 0.0075785 v FourierNb 4.5164e-05 222.08 1.8996 0.09053 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.152 533.98 403.57 422.05 v Boundary Density 0.41072 4.3712 0.98293 0.89722 v Yplus 0 42.956 2.4502 0.95086 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7704e-05 42.729 0.46826 0.010599 INSTANT 0.158767410E-01 TIME STEP NUMBER 30037 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.580489578E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560952328E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125393577E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10370E+01 0.57416E+02 Friction velocity uk : 0.10370E+01 0.57416E+02 Dimensionless distance yplus : 0.20615E-01 0.42968E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14479E-01 0.12424E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60093E+03 3 0.12741E-06 0.84554E+02 0.22230E+03 c Velocity[X] 0.89237E+01 c Velocity[Y] 0.11794E+02 c Velocity[Z] 0.63836E+02 c Pressure 0.75413E-01 5 0.95985E-08 0.53108E+07 0.60652E+02 c k 0.24306E+04 1 0.96317E-06 0.80728E+06 0.45831E+04 c omega 0.81510E+09 1 0.70571E-08 0.24291E+13 0.11414E+03 c TotEner 0.24204E+06 1 0.12154E-05 0.12033E+08 0.37772E+02 c temperature 0.00000E+00 0 0.00000E+00 0.19714E+02 0.35822E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0796e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -221.69 221.7 0.0016045 0.00059538 v Velocity[Y] -0.13052 701.89 250.44 80.911 v Velocity[Z] -19.25 344.19 24.345 1.9448 v ǁVelocityǁ 0.059928 701.9 259.63 83.655 v Pressure 52989 1.1026e+05 1.037e+05 1.0417e+05 v k 1.1871e-08 40712 904.28 355.5 v omega 153.73 9.6775e+09 1.8454e+08 3.414e+05 v TotEner 97718 6.2953e+05 3.4153e+05 2.485e+05 v temperature 71.055 533.98 398.11 337.16 v Density 0.41002 4.3758 0.94982 1.0905 v TurbVisc 8.8429e-19 0.064128 0.010069 0.028622 v CourantNb 1.2257e-05 41.967 0.37911 0.0075787 v FourierNb 4.5162e-05 221.7 1.8981 0.090531 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.104 533.98 403.56 422.04 v Boundary Density 0.41036 4.3735 0.98293 0.89722 v Yplus 0 42.968 2.4499 0.95085 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7723e-05 42.756 0.46851 0.010599 INSTANT 0.158770039E-01 TIME STEP NUMBER 30038 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.581448137E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560935048E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125368441E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10370E+01 0.57430E+02 Friction velocity uk : 0.10370E+01 0.57430E+02 Dimensionless distance yplus : 0.20614E-01 0.42979E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14478E-01 0.12425E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60094E+03 3 0.12690E-06 0.82078E+02 0.21902E+03 c Velocity[X] 0.83361E+01 c Velocity[Y] 0.11766E+02 c Velocity[Z] 0.61976E+02 c Pressure 0.75417E-01 5 0.96475E-08 0.51911E+07 0.59964E+02 c k 0.24309E+04 1 0.95508E-06 0.74758E+06 0.44100E+04 c omega 0.81510E+09 1 0.70075E-08 0.22461E+13 0.10975E+03 c TotEner 0.24204E+06 1 0.12138E-05 0.11632E+08 0.37137E+02 c temperature 0.00000E+00 0 0.00000E+00 0.19224E+02 0.35374E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0777e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -221.79 221.8 0.0015912 0.0005991 v Velocity[Y] -0.13052 701.89 250.45 80.912 v Velocity[Z] -19.25 344.51 24.355 1.945 v ǁVelocityǁ 0.058857 701.9 259.64 83.656 v Pressure 52943 1.1026e+05 1.037e+05 1.0417e+05 v k 1.1869e-08 40707 904.44 355.5 v omega 153.73 9.6776e+09 1.8454e+08 3.414e+05 v TotEner 97681 6.2953e+05 3.4153e+05 2.485e+05 v temperature 71.005 533.98 398.11 337.16 v Density 0.40968 4.3782 0.9498 1.0905 v TurbVisc 8.8413e-19 0.064128 0.010069 0.028622 v CourantNb 1.2268e-05 41.991 0.37932 0.0075789 v FourierNb 4.516e-05 221.34 1.8966 0.090533 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.055 533.98 403.55 422.04 v Boundary Density 0.41002 4.3758 0.98294 0.89723 v Yplus 0 42.979 2.4496 0.95085 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7743e-05 42.782 0.46875 0.010599 INSTANT 0.158772669E-01 TIME STEP NUMBER 30039 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.582457266E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560918169E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125340790E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10369E+01 0.57443E+02 Friction velocity uk : 0.10369E+01 0.57443E+02 Dimensionless distance yplus : 0.20612E-01 0.42990E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14477E-01 0.12425E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60094E+03 3 0.12643E-06 0.80526E+02 0.21694E+03 c Velocity[X] 0.83781E+01 c Velocity[Y] 0.11732E+02 c Velocity[Z] 0.60415E+02 c Pressure 0.75421E-01 5 0.96864E-08 0.50368E+07 0.59066E+02 c k 0.24312E+04 1 0.94665E-06 0.68820E+06 0.42310E+04 c omega 0.81510E+09 1 0.68859E-08 0.21107E+13 0.10639E+03 c TotEner 0.24204E+06 1 0.12122E-05 0.11092E+08 0.36264E+02 c temperature 0.00000E+00 0 0.00000E+00 0.18559E+02 0.34757E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0758e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -221.9 221.91 0.0015797 0.00060284 v Velocity[Y] -0.13051 701.89 250.45 80.913 v Velocity[Z] -19.249 344.82 24.365 1.9452 v ǁVelocityǁ 0.057763 701.9 259.64 83.657 v Pressure 52898 1.1026e+05 1.037e+05 1.0417e+05 v k 1.1867e-08 40702 904.6 355.5 v omega 153.74 9.6776e+09 1.8454e+08 3.414e+05 v TotEner 97644 6.2953e+05 3.4153e+05 2.485e+05 v temperature 70.955 533.98 398.11 337.16 v Density 0.40935 4.3805 0.94978 1.0905 v TurbVisc 8.8398e-19 0.064128 0.010069 0.028623 v CourantNb 1.2281e-05 42.015 0.37953 0.0075791 v FourierNb 4.5158e-05 221 1.8951 0.090534 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 71.005 533.98 403.53 422.04 v Boundary Density 0.40968 4.3782 0.98295 0.89723 v Yplus 0 42.99 2.4494 0.95084 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7762e-05 42.808 0.46898 0.0106 INSTANT 0.158775298E-01 TIME STEP NUMBER 30040 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.583514410E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560901839E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125310104E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10368E+01 0.57456E+02 Friction velocity uk : 0.10368E+01 0.57456E+02 Dimensionless distance yplus : 0.20611E-01 0.43001E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14476E-01 0.12426E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60094E+03 2 0.25612E-06 0.78263E+02 0.21387E+03 c Velocity[X] 0.85765E+01 c Velocity[Y] 0.11489E+02 c Velocity[Z] 0.58197E+02 c Pressure 0.75425E-01 5 0.96066E-08 0.48515E+07 0.57970E+02 c k 0.24314E+04 1 0.93841E-06 0.63035E+06 0.40490E+04 c omega 0.81510E+09 1 0.70411E-08 0.20216E+13 0.10412E+03 c TotEner 0.24204E+06 1 0.12100E-05 0.10477E+08 0.35245E+02 c temperature 0.00000E+00 0 0.00000E+00 0.17734E+02 0.33976E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.074e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -221.97 221.98 0.0015883 0.00060658 v Velocity[Y] -0.13051 701.89 250.45 80.914 v Velocity[Z] -19.248 345.12 24.374 1.9453 v ǁVelocityǁ 0.056645 701.9 259.65 83.657 v Pressure 52854 1.1026e+05 1.037e+05 1.0417e+05 v k 1.1865e-08 40696 904.75 355.5 v omega 153.74 9.6776e+09 1.8454e+08 3.414e+05 v TotEner 97607 6.2953e+05 3.4154e+05 2.485e+05 v temperature 70.904 533.98 398.1 337.16 v Density 0.40903 4.3829 0.94977 1.0905 v TurbVisc 8.8383e-19 0.064128 0.010069 0.028623 v CourantNb 1.2293e-05 42.039 0.37974 0.0075793 v FourierNb 4.5156e-05 220.68 1.8937 0.090536 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.955 533.98 403.52 422.04 v Boundary Density 0.40935 4.3805 0.98296 0.89723 v Yplus 0 43.001 2.4492 0.95084 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7781e-05 42.834 0.46921 0.0106 INSTANT 0.158777927E-01 TIME STEP NUMBER 30041 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.584617022E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560886172E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125275894E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10368E+01 0.57468E+02 Friction velocity uk : 0.10368E+01 0.57468E+02 Dimensionless distance yplus : 0.20610E-01 0.43013E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14475E-01 0.12427E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60094E+03 2 0.25681E-06 0.77406E+02 0.21269E+03 c Velocity[X] 0.89597E+01 c Velocity[Y] 0.11457E+02 c Velocity[Z] 0.56990E+02 c Pressure 0.75429E-01 5 0.97496E-08 0.46771E+07 0.56919E+02 c k 0.24316E+04 1 0.93003E-06 0.57501E+06 0.38669E+04 c omega 0.81510E+09 1 0.71158E-08 0.19674E+13 0.10272E+03 c TotEner 0.24204E+06 1 0.12086E-05 0.98484E+07 0.34171E+02 c temperature 0.00000E+00 0 0.00000E+00 0.16958E+02 0.33224E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0728e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -222.05 222.06 0.0015978 0.00061034 v Velocity[Y] -0.13051 701.89 250.45 80.915 v Velocity[Z] -19.248 345.41 24.384 1.9455 v ǁVelocityǁ 0.055504 701.9 259.66 83.658 v Pressure 52812 1.1026e+05 1.0369e+05 1.0417e+05 v k 1.1864e-08 40691 904.9 355.5 v omega 153.75 9.6776e+09 1.8454e+08 3.414e+05 v TotEner 97568 6.2953e+05 3.4154e+05 2.485e+05 v temperature 70.852 533.98 398.1 337.16 v Density 0.40871 4.3852 0.94975 1.0905 v TurbVisc 8.8369e-19 0.064128 0.010069 0.028623 v CourantNb 1.2307e-05 42.062 0.37992 0.0075794 v FourierNb 4.5154e-05 220.34 1.8928 0.090537 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.904 533.98 403.51 422.04 v Boundary Density 0.40903 4.3829 0.98297 0.89724 v Yplus 0 43.013 2.449 0.95084 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.78e-05 42.851 0.46938 0.0106 INSTANT 0.158780556E-01 TIME STEP NUMBER 30042 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.585762567E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560871269E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125238066E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10367E+01 0.57479E+02 Friction velocity uk : 0.10367E+01 0.57479E+02 Dimensionless distance yplus : 0.20609E-01 0.43024E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14474E-01 0.12427E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60094E+03 2 0.25731E-06 0.76526E+02 0.21148E+03 c Velocity[X] 0.91252E+01 c Velocity[Y] 0.11434E+02 c Velocity[Z] 0.55967E+02 c Pressure 0.75433E-01 9 0.81600E-08 0.45170E+07 0.55936E+02 c k 0.24319E+04 1 0.92204E-06 0.52292E+06 0.36873E+04 c omega 0.81510E+09 1 0.71764E-08 0.18872E+13 0.10060E+03 c TotEner 0.24204E+06 1 0.12071E-05 0.92586E+07 0.33132E+02 c temperature 0.00000E+00 0 0.00000E+00 0.16242E+02 0.32514E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0715e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -222.13 222.14 0.0016077 0.0006141 v Velocity[Y] -0.1305 701.89 250.45 80.916 v Velocity[Z] -19.247 345.69 24.393 1.9457 v ǁVelocityǁ 0.054341 701.9 259.67 83.659 v Pressure 52770 1.1026e+05 1.0369e+05 1.0417e+05 v k 1.1862e-08 40685 905.04 355.5 v omega 153.75 9.6776e+09 1.8454e+08 3.414e+05 v TotEner 97529 6.2953e+05 3.4154e+05 2.485e+05 v temperature 70.799 533.98 398.1 337.16 v Density 0.4084 4.3876 0.94974 1.0905 v TurbVisc 8.8355e-19 0.064128 0.01007 0.028623 v CourantNb 1.2321e-05 42.084 0.38011 0.0075796 v FourierNb 4.5151e-05 220.12 1.8923 0.090539 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.852 533.98 403.5 422.03 v Boundary Density 0.40871 4.3852 0.98298 0.89724 v Yplus 0 43.024 2.4488 0.95085 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7819e-05 42.868 0.46956 0.0106 INSTANT 0.158783186E-01 TIME STEP NUMBER 30043 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.586948532E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560857165E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125195864E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10366E+01 0.57490E+02 Friction velocity uk : 0.10366E+01 0.57490E+02 Dimensionless distance yplus : 0.20608E-01 0.43035E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14473E-01 0.12428E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60095E+03 2 0.25765E-06 0.75438E+02 0.20997E+03 c Velocity[X] 0.89594E+01 c Velocity[Y] 0.11386E+02 c Velocity[Z] 0.55092E+02 c Pressure 0.75437E-01 9 0.81442E-08 0.43792E+07 0.55076E+02 c k 0.24321E+04 1 0.91283E-06 0.47453E+06 0.35123E+04 c omega 0.81510E+09 1 0.74635E-08 0.18908E+13 0.10070E+03 c TotEner 0.24204E+06 1 0.12056E-05 0.87328E+07 0.32177E+02 c temperature 0.00000E+00 0 0.00000E+00 0.15618E+02 0.31884E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0703e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -222.21 222.23 0.0016174 0.00061788 v Velocity[Y] -0.1305 701.89 250.45 80.917 v Velocity[Z] -19.247 345.97 24.402 1.9458 v ǁVelocityǁ 0.053156 701.9 259.67 83.66 v Pressure 52729 1.1026e+05 1.0369e+05 1.0417e+05 v k 1.1861e-08 40681 905.17 355.5 v omega 153.76 9.6776e+09 1.8454e+08 3.414e+05 v TotEner 97489 6.2953e+05 3.4154e+05 2.485e+05 v temperature 70.745 533.98 398.09 337.16 v Density 0.4081 4.3899 0.94972 1.0905 v TurbVisc 8.8344e-19 0.064128 0.01007 0.028623 v CourantNb 1.2337e-05 42.106 0.38028 0.0075798 v FourierNb 4.5149e-05 219.99 1.8921 0.09054 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.799 533.98 403.48 422.03 v Boundary Density 0.4084 4.3876 0.98299 0.89725 v Yplus 0 43.035 2.4486 0.95086 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7838e-05 42.885 0.46974 0.010601 INSTANT 0.158785815E-01 TIME STEP NUMBER 30044 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.588172414E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560843918E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125148930E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10366E+01 0.57500E+02 Friction velocity uk : 0.10366E+01 0.57500E+02 Dimensionless distance yplus : 0.20606E-01 0.43047E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14472E-01 0.12428E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60095E+03 2 0.25787E-06 0.74179E+02 0.20821E+03 c Velocity[X] 0.84896E+01 c Velocity[Y] 0.11366E+02 c Velocity[Z] 0.54323E+02 c Pressure 0.75441E-01 5 0.99323E-08 0.42623E+07 0.54336E+02 c k 0.24323E+04 1 0.90537E-06 0.43027E+06 0.33443E+04 c omega 0.81510E+09 1 0.71957E-08 0.17140E+13 0.95875E+02 c TotEner 0.24205E+06 1 0.12042E-05 0.82950E+07 0.31361E+02 c temperature 0.00000E+00 0 0.00000E+00 0.15094E+02 0.31344E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.069e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -222.3 222.31 0.0016269 0.00062167 v Velocity[Y] -0.13049 701.89 250.45 80.918 v Velocity[Z] -19.246 346.24 24.411 1.946 v ǁVelocityǁ 0.051949 701.9 259.68 83.661 v Pressure 52689 1.1026e+05 1.0369e+05 1.0417e+05 v k 1.1859e-08 40678 905.31 355.5 v omega 153.76 9.6776e+09 1.8455e+08 3.4141e+05 v TotEner 97448 6.2953e+05 3.4154e+05 2.485e+05 v temperature 70.69 533.98 398.09 337.16 v Density 0.4078 4.3923 0.94971 1.0905 v TurbVisc 8.8333e-19 0.064128 0.01007 0.028624 v CourantNb 1.2352e-05 42.128 0.38046 0.00758 v FourierNb 4.5147e-05 219.92 1.8919 0.090542 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.745 533.98 403.47 422.03 v Boundary Density 0.4081 4.3899 0.98301 0.89725 v Yplus 0 43.047 2.4485 0.95088 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7857e-05 42.903 0.46992 0.010601 INSTANT 0.158788444E-01 TIME STEP NUMBER 30045 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.589431726E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560831601E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125096959E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10365E+01 0.57511E+02 Friction velocity uk : 0.10365E+01 0.57511E+02 Dimensionless distance yplus : 0.20605E-01 0.43058E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14472E-01 0.12429E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60095E+03 2 0.25800E-06 0.72827E+02 0.20630E+03 c Velocity[X] 0.78377E+01 c Velocity[Y] 0.11368E+02 c Velocity[Z] 0.53622E+02 c Pressure 0.75445E-01 5 0.97016E-08 0.41597E+07 0.53678E+02 c k 0.24325E+04 1 0.89991E-06 0.39016E+06 0.31844E+04 c omega 0.81510E+09 1 0.69312E-08 0.15565E+13 0.91364E+02 c TotEner 0.24205E+06 1 0.12028E-05 0.79394E+07 0.30681E+02 c temperature 0.00000E+00 0 0.00000E+00 0.14652E+02 0.30882E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0677e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -222.38 222.39 0.0016363 0.00062546 v Velocity[Y] -0.13049 701.89 250.45 80.919 v Velocity[Z] -19.246 346.5 24.42 1.9462 v ǁVelocityǁ 0.050721 701.9 259.69 83.662 v Pressure 52649 1.1026e+05 1.0368e+05 1.0417e+05 v k 1.1857e-08 40676 905.44 355.5 v omega 153.77 9.6776e+09 1.8455e+08 3.4141e+05 v TotEner 97406 6.2953e+05 3.4154e+05 2.485e+05 v temperature 70.634 533.98 398.09 337.16 v Density 0.40751 4.3947 0.94969 1.0905 v TurbVisc 8.8319e-19 0.064128 0.01007 0.028624 v CourantNb 1.2369e-05 42.15 0.38064 0.0075802 v FourierNb 4.5145e-05 219.89 1.8917 0.090543 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.69 533.98 403.46 422.03 v Boundary Density 0.4078 4.3923 0.98302 0.89725 v Yplus 0 43.058 2.4484 0.9509 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7875e-05 42.921 0.4701 0.010601 INSTANT 0.158791074E-01 TIME STEP NUMBER 30046 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.590724008E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560820234E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.125039711E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10365E+01 0.57522E+02 Friction velocity uk : 0.10365E+01 0.57522E+02 Dimensionless distance yplus : 0.20604E-01 0.43069E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14471E-01 0.12430E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60095E+03 2 0.25806E-06 0.71439E+02 0.20432E+03 c Velocity[X] 0.71559E+01 c Velocity[Y] 0.11327E+02 c Velocity[Z] 0.52955E+02 c Pressure 0.75449E-01 5 0.97907E-08 0.40635E+07 0.53054E+02 c k 0.24328E+04 1 0.89253E-06 0.35379E+06 0.30322E+04 c omega 0.81511E+09 1 0.66752E-08 0.14911E+13 0.89422E+02 c TotEner 0.24205E+06 1 0.12014E-05 0.76385E+07 0.30094E+02 c temperature 0.00000E+00 0 0.00000E+00 0.14265E+02 0.30472E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0664e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -222.46 222.47 0.0016455 0.00062926 v Velocity[Y] -0.13048 701.89 250.45 80.919 v Velocity[Z] -19.245 346.75 24.429 1.9464 v ǁVelocityǁ 0.049474 701.9 259.69 83.663 v Pressure 52610 1.1025e+05 1.0368e+05 1.0417e+05 v k 1.1856e-08 40675 905.57 355.5 v omega 153.77 9.6776e+09 1.8455e+08 3.4141e+05 v TotEner 97363 6.2953e+05 3.4154e+05 2.485e+05 v temperature 70.577 533.98 398.08 337.16 v Density 0.40722 4.3971 0.94968 1.0904 v TurbVisc 8.8306e-19 0.064128 0.01007 0.028624 v CourantNb 1.2386e-05 42.171 0.38082 0.0075804 v FourierNb 4.5143e-05 219.87 1.8914 0.090545 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.634 533.98 403.45 422.03 v Boundary Density 0.40751 4.3947 0.98304 0.89726 v Yplus 0 43.069 2.4483 0.95092 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7894e-05 42.939 0.47028 0.010601 INSTANT 0.158793703E-01 TIME STEP NUMBER 30047 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.592046812E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560809803E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124977011E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10364E+01 0.57532E+02 Friction velocity uk : 0.10364E+01 0.57532E+02 Dimensionless distance yplus : 0.20603E-01 0.43080E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14471E-01 0.12430E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60095E+03 2 0.25808E-06 0.70191E+02 0.20253E+03 c Velocity[X] 0.65706E+01 c Velocity[Y] 0.11315E+02 c Velocity[Z] 0.52305E+02 c Pressure 0.75453E-01 5 0.89613E-08 0.39655E+07 0.52410E+02 c k 0.24330E+04 1 0.88839E-06 0.32119E+06 0.28889E+04 c omega 0.81511E+09 1 0.64873E-08 0.13996E+13 0.86636E+02 c TotEner 0.24205E+06 1 0.12000E-05 0.74009E+07 0.29622E+02 c temperature 0.00000E+00 0 0.00000E+00 0.13921E+02 0.30102E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0651e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -222.54 222.55 0.0016547 0.00063308 v Velocity[Y] -0.13048 701.89 250.46 80.92 v Velocity[Z] -19.244 347 24.438 1.9465 v ǁVelocityǁ 0.048207 701.9 259.7 83.664 v Pressure 52571 1.1025e+05 1.0368e+05 1.0417e+05 v k 1.1854e-08 40675 905.69 355.5 v omega 153.78 9.6777e+09 1.8455e+08 3.4141e+05 v TotEner 97320 6.2953e+05 3.4154e+05 2.485e+05 v temperature 70.52 533.98 398.08 337.16 v Density 0.40693 4.3995 0.94967 1.0904 v TurbVisc 8.8294e-19 0.064128 0.01007 0.028624 v CourantNb 1.2414e-05 42.193 0.38099 0.0075806 v FourierNb 4.5142e-05 219.84 1.891 0.090546 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.577 533.98 403.44 422.03 v Boundary Density 0.40722 4.3971 0.98306 0.89727 v Yplus 0 43.08 2.4483 0.95095 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7913e-05 42.957 0.47047 0.010602 INSTANT 0.158796332E-01 TIME STEP NUMBER 30048 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.593397718E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560800338E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124908752E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10364E+01 0.57543E+02 Friction velocity uk : 0.10364E+01 0.57543E+02 Dimensionless distance yplus : 0.20602E-01 0.43092E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14470E-01 0.12431E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60096E+03 2 0.25806E-06 0.69124E+02 0.20098E+03 c Velocity[X] 0.61494E+01 c Velocity[Y] 0.11319E+02 c Velocity[Z] 0.51656E+02 c Pressure 0.75457E-01 5 0.89908E-08 0.38618E+07 0.51721E+02 c k 0.24332E+04 1 0.88586E-06 0.29194E+06 0.27540E+04 c omega 0.81511E+09 1 0.64316E-08 0.13057E+13 0.83680E+02 c TotEner 0.24205E+06 1 0.11987E-05 0.72107E+07 0.29239E+02 c temperature 0.00000E+00 0 0.00000E+00 0.13605E+02 0.29758E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0638e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -222.61 222.63 0.0016637 0.00063689 v Velocity[Y] -0.13047 701.9 250.46 80.921 v Velocity[Z] -19.244 347.25 24.447 1.9467 v ǁVelocityǁ 0.046923 701.9 259.71 83.665 v Pressure 52533 1.1025e+05 1.0368e+05 1.0417e+05 v k 1.1853e-08 40676 905.81 355.5 v omega 153.78 9.6777e+09 1.8455e+08 3.4141e+05 v TotEner 97275 6.2953e+05 3.4154e+05 2.485e+05 v temperature 70.461 533.98 398.08 337.16 v Density 0.40665 4.402 0.94965 1.0904 v TurbVisc 8.8282e-19 0.064128 0.01007 0.028624 v CourantNb 1.2444e-05 42.214 0.38116 0.0075807 v FourierNb 4.514e-05 219.8 1.8905 0.090547 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.52 533.98 403.43 422.02 v Boundary Density 0.40693 4.3995 0.98308 0.89727 v Yplus 0 43.092 2.4482 0.95099 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7924e-05 42.976 0.47065 0.010602 INSTANT 0.158798962E-01 TIME STEP NUMBER 30049 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.594774329E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560791835E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124834898E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10363E+01 0.57553E+02 Friction velocity uk : 0.10363E+01 0.57553E+02 Dimensionless distance yplus : 0.20601E-01 0.43103E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14469E-01 0.12432E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60096E+03 2 0.25801E-06 0.68193E+02 0.19962E+03 c Velocity[X] 0.58964E+01 c Velocity[Y] 0.11297E+02 c Velocity[Z] 0.51000E+02 c Pressure 0.75461E-01 5 0.95065E-08 0.37522E+07 0.50981E+02 c k 0.24335E+04 1 0.88219E-06 0.26558E+06 0.26266E+04 c omega 0.81511E+09 1 0.64108E-08 0.12607E+13 0.82222E+02 c TotEner 0.24205E+06 1 0.11973E-05 0.70503E+07 0.28912E+02 c temperature 0.00000E+00 0 0.00000E+00 0.13312E+02 0.29436E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0625e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -222.69 222.7 0.0016722 0.0006407 v Velocity[Y] -0.13047 701.9 250.46 80.922 v Velocity[Z] -19.243 347.49 24.456 1.9469 v ǁVelocityǁ 0.045621 701.9 259.71 83.666 v Pressure 52495 1.1025e+05 1.0367e+05 1.0417e+05 v k 1.1851e-08 40677 905.93 355.49 v omega 153.79 9.6777e+09 1.8455e+08 3.4141e+05 v TotEner 97230 6.2953e+05 3.4154e+05 2.485e+05 v temperature 70.402 533.98 398.08 337.16 v Density 0.40637 4.4044 0.94964 1.0904 v TurbVisc 8.8271e-19 0.064128 0.01007 0.028625 v CourantNb 1.2474e-05 42.235 0.38133 0.0075809 v FourierNb 4.5138e-05 219.72 1.8899 0.090549 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.461 533.98 403.42 422.02 v Boundary Density 0.40665 4.402 0.9831 0.89728 v Yplus 0 43.103 2.4482 0.95102 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7918e-05 42.994 0.47082 0.010602 INSTANT 0.158801591E-01 TIME STEP NUMBER 30050 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.596174274E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560784276E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124755488E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10363E+01 0.57563E+02 Friction velocity uk : 0.10363E+01 0.57563E+02 Dimensionless distance yplus : 0.20600E-01 0.43115E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14468E-01 0.12432E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60096E+03 2 0.25795E-06 0.67380E+02 0.19842E+03 c Velocity[X] 0.57691E+01 c Velocity[Y] 0.11275E+02 c Velocity[Z] 0.50336E+02 c Pressure 0.75465E-01 5 0.94768E-08 0.36388E+07 0.50205E+02 c k 0.24337E+04 1 0.87946E-06 0.24180E+06 0.25061E+04 c omega 0.81511E+09 1 0.64250E-08 0.12293E+13 0.81192E+02 c TotEner 0.24205E+06 1 0.11960E-05 0.69208E+07 0.28645E+02 c temperature 0.00000E+00 0 0.00000E+00 0.13047E+02 0.29141E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0612e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -222.77 222.78 0.0016802 0.0006445 v Velocity[Y] -0.13046 701.9 250.46 80.923 v Velocity[Z] -19.243 347.73 24.464 1.947 v ǁVelocityǁ 0.044303 701.9 259.72 83.667 v Pressure 52457 1.1025e+05 1.0367e+05 1.0417e+05 v k 1.185e-08 40679 906.04 355.49 v omega 153.79 9.6777e+09 1.8455e+08 3.4141e+05 v TotEner 97184 6.2953e+05 3.4154e+05 2.485e+05 v temperature 70.341 533.98 398.07 337.16 v Density 0.4061 4.4069 0.94963 1.0904 v TurbVisc 8.826e-19 0.064128 0.01007 0.028625 v CourantNb 1.2506e-05 42.256 0.3815 0.0075811 v FourierNb 4.5136e-05 219.63 1.8892 0.09055 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.402 533.98 403.4 422.02 v Boundary Density 0.40637 4.4044 0.98313 0.89728 v Yplus 0 43.115 2.4481 0.95106 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7912e-05 43.013 0.471 0.010602 INSTANT 0.158804220E-01 TIME STEP NUMBER 30051 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.597595206E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560777629E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124670629E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10362E+01 0.57573E+02 Friction velocity uk : 0.10362E+01 0.57573E+02 Dimensionless distance yplus : 0.20599E-01 0.43126E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14468E-01 0.12433E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60096E+03 2 0.25787E-06 0.66621E+02 0.19730E+03 c Velocity[X] 0.57050E+01 c Velocity[Y] 0.11250E+02 c Velocity[Z] 0.49666E+02 c Pressure 0.75469E-01 5 0.94603E-08 0.35256E+07 0.49418E+02 c k 0.24340E+04 1 0.87732E-06 0.22029E+06 0.23918E+04 c omega 0.81511E+09 1 0.65288E-08 0.11953E+13 0.80063E+02 c TotEner 0.24206E+06 1 0.11946E-05 0.68153E+07 0.28426E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12810E+02 0.28876E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0599e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -222.84 222.85 0.0016876 0.00064829 v Velocity[Y] -0.13046 701.9 250.46 80.924 v Velocity[Z] -19.242 347.96 24.473 1.9472 v ǁVelocityǁ 0.042971 701.9 259.73 83.667 v Pressure 52420 1.1025e+05 1.0367e+05 1.0417e+05 v k 1.1848e-08 40681 906.15 355.49 v omega 153.8 9.6777e+09 1.8455e+08 3.4141e+05 v TotEner 97137 6.2953e+05 3.4154e+05 2.485e+05 v temperature 70.28 533.98 398.07 337.16 v Density 0.40583 4.4094 0.94962 1.0904 v TurbVisc 8.8249e-19 0.064127 0.01007 0.028625 v CourantNb 1.2539e-05 42.277 0.38167 0.0075812 v FourierNb 4.5134e-05 219.5 1.8884 0.090551 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.341 533.98 403.39 422.02 v Boundary Density 0.4061 4.4069 0.98315 0.89729 v Yplus 0 43.126 2.4481 0.9511 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7906e-05 43.031 0.47118 0.010603 INSTANT 0.158806850E-01 TIME STEP NUMBER 30052 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.599034811E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560771858E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124580499E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10362E+01 0.57583E+02 Friction velocity uk : 0.10362E+01 0.57583E+02 Dimensionless distance yplus : 0.20598E-01 0.43138E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14467E-01 0.12433E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60096E+03 2 0.25778E-06 0.65879E+02 0.19620E+03 c Velocity[X] 0.56469E+01 c Velocity[Y] 0.11239E+02 c Velocity[Z] 0.48994E+02 c Pressure 0.75473E-01 5 0.92501E-08 0.34162E+07 0.48645E+02 c k 0.24342E+04 1 0.87683E-06 0.20083E+06 0.22836E+04 c omega 0.81511E+09 1 0.64816E-08 0.11499E+13 0.78528E+02 c TotEner 0.24206E+06 1 0.11932E-05 0.67311E+07 0.28250E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12602E+02 0.28640E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0586e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -222.92 222.93 0.0016944 0.00065207 v Velocity[Y] -0.13046 701.9 250.46 80.925 v Velocity[Z] -19.242 348.18 24.481 1.9474 v ǁVelocityǁ 0.041626 701.9 259.73 83.668 v Pressure 52384 1.1025e+05 1.0367e+05 1.0417e+05 v k 1.1847e-08 40684 906.26 355.49 v omega 153.8 9.6777e+09 1.8456e+08 3.4141e+05 v TotEner 97089 6.2952e+05 3.4154e+05 2.485e+05 v temperature 70.218 533.98 398.07 337.16 v Density 0.40556 4.412 0.94961 1.0904 v TurbVisc 8.8239e-19 0.064127 0.01007 0.028625 v CourantNb 1.2572e-05 42.297 0.38183 0.0075814 v FourierNb 4.5132e-05 219.36 1.8876 0.090552 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.28 533.98 403.38 422.02 v Boundary Density 0.40583 4.4094 0.98317 0.8973 v Yplus 0 43.138 2.448 0.95114 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.79e-05 43.05 0.47135 0.010603 INSTANT 0.158809479E-01 TIME STEP NUMBER 30053 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.600490801E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560766911E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124485344E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10361E+01 0.57593E+02 Friction velocity uk : 0.10361E+01 0.57593E+02 Dimensionless distance yplus : 0.20597E-01 0.43149E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14466E-01 0.12434E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60096E+03 2 0.25767E-06 0.65115E+02 0.19506E+03 c Velocity[X] 0.55595E+01 c Velocity[Y] 0.11230E+02 c Velocity[Z] 0.48326E+02 c Pressure 0.75477E-01 5 0.92505E-08 0.33132E+07 0.47906E+02 c k 0.24345E+04 1 0.87787E-06 0.18321E+06 0.21809E+04 c omega 0.81511E+09 1 0.61010E-08 0.10620E+13 0.75465E+02 c TotEner 0.24206E+06 1 0.11918E-05 0.66570E+07 0.28094E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12416E+02 0.28428E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0573e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -222.99 223 0.0017004 0.00065585 v Velocity[Y] -0.13045 701.9 250.46 80.926 v Velocity[Z] -19.241 348.41 24.49 1.9476 v ǁVelocityǁ 0.040271 701.9 259.74 83.669 v Pressure 52348 1.1025e+05 1.0367e+05 1.0417e+05 v k 1.1846e-08 40687 906.37 355.49 v omega 153.8 9.6777e+09 1.8456e+08 3.4141e+05 v TotEner 97041 6.2952e+05 3.4154e+05 2.485e+05 v temperature 70.156 533.98 398.07 337.16 v Density 0.4053 4.4145 0.94959 1.0904 v TurbVisc 8.823e-19 0.064127 0.01007 0.028625 v CourantNb 1.2606e-05 42.317 0.382 0.0075816 v FourierNb 4.513e-05 219.2 1.8868 0.090553 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.218 533.98 403.37 422.02 v Boundary Density 0.40556 4.412 0.9832 0.8973 v Yplus 0 43.149 2.448 0.95118 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7893e-05 43.068 0.47152 0.010603 INSTANT 0.158812109E-01 TIME STEP NUMBER 30054 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.601960921E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560762730E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124385473E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10361E+01 0.57603E+02 Friction velocity uk : 0.10361E+01 0.57603E+02 Dimensionless distance yplus : 0.20596E-01 0.43161E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14466E-01 0.12435E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60097E+03 2 0.25755E-06 0.64324E+02 0.19386E+03 c Velocity[X] 0.54334E+01 c Velocity[Y] 0.11222E+02 c Velocity[Z] 0.47668E+02 c Pressure 0.75481E-01 5 0.91175E-08 0.32168E+07 0.47205E+02 c k 0.24347E+04 1 0.88031E-06 0.16724E+06 0.20836E+04 c omega 0.81511E+09 1 0.70099E-08 0.11652E+13 0.79048E+02 c TotEner 0.24206E+06 1 0.11904E-05 0.65829E+07 0.27937E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12241E+02 0.28227E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.056e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -223.06 223.07 0.0017056 0.00065961 v Velocity[Y] -0.13045 701.9 250.46 80.927 v Velocity[Z] -19.241 348.63 24.498 1.9477 v ǁVelocityǁ 0.038907 701.9 259.75 83.67 v Pressure 52312 1.1025e+05 1.0366e+05 1.0417e+05 v k 1.1845e-08 40689 906.47 355.49 v omega 153.81 9.6777e+09 1.8456e+08 3.4141e+05 v TotEner 96992 6.2952e+05 3.4154e+05 2.485e+05 v temperature 70.093 533.98 398.06 337.16 v Density 0.40504 4.4172 0.94958 1.0904 v TurbVisc 8.822e-19 0.064127 0.01007 0.028625 v CourantNb 1.2642e-05 42.337 0.38216 0.0075817 v FourierNb 4.5129e-05 219.02 1.886 0.090554 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.156 533.98 403.36 422.01 v Boundary Density 0.4053 4.4145 0.98322 0.89731 v Yplus 0 43.161 2.448 0.95121 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7894e-05 43.086 0.47169 0.010603 INSTANT 0.158814738E-01 TIME STEP NUMBER 30055 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.603442948E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560759255E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124281255E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10361E+01 0.57612E+02 Friction velocity uk : 0.10361E+01 0.57612E+02 Dimensionless distance yplus : 0.20595E-01 0.43173E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14465E-01 0.12435E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60097E+03 2 0.25741E-06 0.63526E+02 0.19266E+03 c Velocity[X] 0.52802E+01 c Velocity[Y] 0.11220E+02 c Velocity[Z] 0.47026E+02 c Pressure 0.75485E-01 5 0.90442E-08 0.31265E+07 0.46537E+02 c k 0.24350E+04 1 0.88430E-06 0.15282E+06 0.19916E+04 c omega 0.81511E+09 1 0.65106E-08 0.10329E+13 0.74425E+02 c TotEner 0.24206E+06 1 0.11890E-05 0.65017E+07 0.27764E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12066E+02 0.28024E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0547e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -223.13 223.15 0.0017102 0.00066336 v Velocity[Y] -0.13044 701.9 250.46 80.928 v Velocity[Z] -19.24 348.84 24.507 1.9479 v ǁVelocityǁ 0.037538 701.9 259.75 83.671 v Pressure 52277 1.1025e+05 1.0366e+05 1.0417e+05 v k 1.1843e-08 40693 906.57 355.49 v omega 153.81 9.6777e+09 1.8456e+08 3.4141e+05 v TotEner 96943 6.2952e+05 3.4154e+05 2.485e+05 v temperature 70.029 533.98 398.06 337.16 v Density 0.40478 4.4198 0.94957 1.0904 v TurbVisc 8.8211e-19 0.064127 0.01007 0.028626 v CourantNb 1.2678e-05 42.357 0.38232 0.0075819 v FourierNb 4.5127e-05 218.84 1.8852 0.090555 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.093 533.98 403.35 422.01 v Boundary Density 0.40504 4.4172 0.98325 0.89732 v Yplus 0 43.173 2.4479 0.95125 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7902e-05 43.104 0.47186 0.010604 INSTANT 0.158817368E-01 TIME STEP NUMBER 30056 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.604934693E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560756417E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124173113E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10360E+01 0.57622E+02 Friction velocity uk : 0.10360E+01 0.57622E+02 Dimensionless distance yplus : 0.20595E-01 0.43185E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14464E-01 0.12436E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60097E+03 2 0.25727E-06 0.62743E+02 0.19147E+03 c Velocity[X] 0.51214E+01 c Velocity[Y] 0.11219E+02 c Velocity[Z] 0.46403E+02 c Pressure 0.75489E-01 5 0.91606E-08 0.30409E+07 0.45896E+02 c k 0.24352E+04 1 0.89056E-06 0.13989E+06 0.19053E+04 c omega 0.81511E+09 1 0.63071E-08 0.94770E+12 0.71289E+02 c TotEner 0.24206E+06 1 0.11876E-05 0.64065E+07 0.27560E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11879E+02 0.27806E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0535e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -223.2 223.22 0.0017139 0.0006671 v Velocity[Y] -0.13044 701.9 250.46 80.929 v Velocity[Z] -19.239 349.05 24.515 1.9481 v ǁVelocityǁ 0.036167 701.9 259.76 83.672 v Pressure 52243 1.1025e+05 1.0366e+05 1.0417e+05 v k 1.1842e-08 40696 906.67 355.49 v omega 153.82 9.6777e+09 1.8456e+08 3.4141e+05 v TotEner 96893 6.2952e+05 3.4155e+05 2.485e+05 v temperature 69.966 533.97 398.06 337.16 v Density 0.40453 4.4225 0.94956 1.0904 v TurbVisc 8.8202e-19 0.064127 0.01007 0.028626 v CourantNb 1.2714e-05 42.376 0.38247 0.007582 v FourierNb 4.5125e-05 218.64 1.8843 0.090556 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 70.029 533.98 403.34 422.01 v Boundary Density 0.40478 4.4198 0.98327 0.89732 v Yplus 0 43.185 2.4479 0.95129 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.791e-05 43.122 0.47203 0.010604 INSTANT 0.158819997E-01 TIME STEP NUMBER 30057 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.606434002E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560754150E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124061517E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10360E+01 0.57631E+02 Friction velocity uk : 0.10360E+01 0.57631E+02 Dimensionless distance yplus : 0.20594E-01 0.43198E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14464E-01 0.12437E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60097E+03 2 0.25712E-06 0.62028E+02 0.19037E+03 c Velocity[X] 0.49775E+01 c Velocity[Y] 0.11250E+02 c Velocity[Z] 0.45801E+02 c Pressure 0.75493E-01 5 0.95269E-08 0.29587E+07 0.45271E+02 c k 0.24355E+04 1 0.90003E-06 0.12843E+06 0.18255E+04 c omega 0.81511E+09 1 0.62574E-08 0.95185E+12 0.71445E+02 c TotEner 0.24206E+06 1 0.11863E-05 0.63026E+07 0.27335E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11676E+02 0.27568E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0522e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -223.27 223.29 0.0017166 0.00067082 v Velocity[Y] -0.13043 701.9 250.46 80.93 v Velocity[Z] -19.239 349.26 24.523 1.9483 v ǁVelocityǁ 0.034797 701.9 259.77 83.673 v Pressure 52209 1.1025e+05 1.0366e+05 1.0417e+05 v k 1.1841e-08 40700 906.76 355.49 v omega 153.82 9.6777e+09 1.8456e+08 3.4141e+05 v TotEner 96842 6.2952e+05 3.4155e+05 2.485e+05 v temperature 69.901 533.97 398.06 337.16 v Density 0.40428 4.4253 0.94955 1.0904 v TurbVisc 8.8194e-19 0.064127 0.01007 0.028626 v CourantNb 1.2752e-05 42.395 0.38263 0.0075822 v FourierNb 4.5124e-05 218.45 1.8835 0.090557 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 69.966 533.97 403.33 422.01 v Boundary Density 0.40453 4.4225 0.9833 0.89733 v Yplus 0 43.198 2.4478 0.95132 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7919e-05 43.139 0.4722 0.010604 INSTANT 0.158822626E-01 TIME STEP NUMBER 30058 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.607938757E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560752351E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123946980E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10359E+01 0.57640E+02 Friction velocity uk : 0.10359E+01 0.57640E+02 Dimensionless distance yplus : 0.20593E-01 0.43210E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14463E-01 0.12437E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60097E+03 2 0.25696E-06 0.61368E+02 0.18935E+03 c Velocity[X] 0.48612E+01 c Velocity[Y] 0.11288E+02 c Velocity[Z] 0.45219E+02 c Pressure 0.75497E-01 9 0.97032E-08 0.28787E+07 0.44655E+02 c k 0.24357E+04 1 0.90993E-06 0.11831E+06 0.17520E+04 c omega 0.81511E+09 1 0.62550E-08 0.95636E+12 0.71614E+02 c TotEner 0.24207E+06 1 0.11849E-05 0.61815E+07 0.27072E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11452E+02 0.27302E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.051e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -223.34 223.35 0.0017187 0.00067452 v Velocity[Y] -0.13043 701.9 250.47 80.931 v Velocity[Z] -19.238 349.47 24.531 1.9484 v ǁVelocityǁ 0.033433 701.9 259.77 83.674 v Pressure 52175 1.1025e+05 1.0366e+05 1.0417e+05 v k 1.184e-08 40704 906.85 355.49 v omega 153.83 9.6778e+09 1.8456e+08 3.4141e+05 v TotEner 96792 6.2952e+05 3.4155e+05 2.485e+05 v temperature 69.837 533.97 398.05 337.16 v Density 0.40403 4.4281 0.94954 1.0904 v TurbVisc 8.8185e-19 0.064127 0.01007 0.028626 v CourantNb 1.279e-05 42.414 0.38278 0.0075824 v FourierNb 4.5122e-05 218.25 1.8826 0.090557 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 69.901 533.97 403.32 422.01 v Boundary Density 0.40428 4.4253 0.98333 0.89734 v Yplus 0 43.21 2.4478 0.95136 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7927e-05 43.157 0.47236 0.010604 INSTANT 0.158825256E-01 TIME STEP NUMBER 30059 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.609446877E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560750955E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123830049E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10359E+01 0.57649E+02 Friction velocity uk : 0.10359E+01 0.57649E+02 Dimensionless distance yplus : 0.20592E-01 0.43223E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14462E-01 0.12438E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60098E+03 2 0.25680E-06 0.60649E+02 0.18824E+03 c Velocity[X] 0.47738E+01 c Velocity[Y] 0.11222E+02 c Velocity[Z] 0.44654E+02 c Pressure 0.75501E-01 10 0.92366E-08 0.28012E+07 0.44050E+02 c k 0.24359E+04 1 0.91254E-06 0.10922E+06 0.16832E+04 c omega 0.81511E+09 1 0.59808E-08 0.89553E+12 0.69299E+02 c TotEner 0.24207E+06 1 0.11832E-05 0.60168E+07 0.26708E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11201E+02 0.27001E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0498e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -223.41 223.42 0.0017196 0.00067819 v Velocity[Y] -0.13043 701.9 250.47 80.932 v Velocity[Z] -19.238 349.67 24.539 1.9486 v ǁVelocityǁ 0.03208 701.9 259.78 83.675 v Pressure 52142 1.1025e+05 1.0365e+05 1.0417e+05 v k 1.184e-08 40709 906.94 355.49 v omega 153.83 9.6778e+09 1.8456e+08 3.4141e+05 v TotEner 96741 6.2952e+05 3.4155e+05 2.4851e+05 v temperature 69.772 533.97 398.05 337.17 v Density 0.40379 4.431 0.94953 1.0904 v TurbVisc 8.8179e-19 0.064127 0.01007 0.028626 v CourantNb 1.2819e-05 42.433 0.38293 0.0075825 v FourierNb 4.512e-05 218.04 1.8818 0.090558 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 69.837 533.97 403.31 422.01 v Boundary Density 0.40403 4.4281 0.98336 0.89734 v Yplus 0 43.223 2.4478 0.95139 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7935e-05 43.174 0.47253 0.010604 INSTANT 0.158827885E-01 TIME STEP NUMBER 30060 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.610956322E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560749904E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123711302E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10358E+01 0.57658E+02 Friction velocity uk : 0.10358E+01 0.57658E+02 Dimensionless distance yplus : 0.20591E-01 0.43236E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14462E-01 0.12439E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60098E+03 2 0.25663E-06 0.60015E+02 0.18725E+03 c Velocity[X] 0.47078E+01 c Velocity[Y] 0.11204E+02 c Velocity[Z] 0.44103E+02 c Pressure 0.75505E-01 9 0.87332E-08 0.27265E+07 0.43458E+02 c k 0.24362E+04 1 0.91949E-06 0.10147E+06 0.16223E+04 c omega 0.81511E+09 1 0.56912E-08 0.80854E+12 0.65847E+02 c TotEner 0.24207E+06 1 0.11816E-05 0.58583E+07 0.26354E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10941E+02 0.26686E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0485e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -223.48 223.49 0.0017195 0.00068183 v Velocity[Y] -0.13042 701.9 250.47 80.933 v Velocity[Z] -19.237 349.86 24.547 1.9488 v ǁVelocityǁ 0.030746 701.9 259.78 83.676 v Pressure 52109 1.1025e+05 1.0365e+05 1.0417e+05 v k 1.1839e-08 40715 907.03 355.49 v omega 153.84 9.6778e+09 1.8456e+08 3.4141e+05 v TotEner 96690 6.2952e+05 3.4155e+05 2.4851e+05 v temperature 69.707 533.97 398.05 337.17 v Density 0.40355 4.4339 0.94952 1.0904 v TurbVisc 8.8173e-19 0.064127 0.010069 0.028626 v CourantNb 1.2825e-05 42.451 0.38308 0.0075827 v FourierNb 4.5119e-05 217.84 1.8809 0.090559 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 69.772 533.97 403.3 422.01 v Boundary Density 0.40379 4.431 0.98339 0.89735 v Yplus 0 43.236 2.4477 0.95143 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7944e-05 43.191 0.47269 0.010605 INSTANT 0.158830515E-01 TIME STEP NUMBER 30061 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.612465090E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560749127E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123591334E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10358E+01 0.57667E+02 Friction velocity uk : 0.10358E+01 0.57667E+02 Dimensionless distance yplus : 0.20590E-01 0.43249E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14461E-01 0.12440E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60098E+03 2 0.25646E-06 0.59405E+02 0.18629E+03 c Velocity[X] 0.46512E+01 c Velocity[Y] 0.11190E+02 c Velocity[Z] 0.43564E+02 c Pressure 0.75509E-01 9 0.83799E-08 0.26557E+07 0.42890E+02 c k 0.24364E+04 1 0.92887E-06 0.94943E+05 0.15692E+04 c omega 0.81511E+09 1 0.55822E-08 0.77462E+12 0.64451E+02 c TotEner 0.24207E+06 1 0.11800E-05 0.56964E+07 0.25988E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10676E+02 0.26361E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0473e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -223.55 223.56 0.0017184 0.00068544 v Velocity[Y] -0.13042 701.9 250.47 80.934 v Velocity[Z] -19.237 350.06 24.555 1.949 v ǁVelocityǁ 0.029436 701.9 259.79 83.677 v Pressure 52077 1.1025e+05 1.0365e+05 1.0417e+05 v k 1.1838e-08 40721 907.11 355.49 v omega 153.84 9.6778e+09 1.8456e+08 3.4141e+05 v TotEner 96639 6.2952e+05 3.4155e+05 2.4851e+05 v temperature 69.642 533.97 398.05 337.17 v Density 0.40331 4.4369 0.94951 1.0904 v TurbVisc 8.8167e-19 0.064127 0.010069 0.028627 v CourantNb 1.2831e-05 42.469 0.38323 0.0075829 v FourierNb 4.5117e-05 217.63 1.8801 0.09056 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 69.707 533.97 403.29 422 v Boundary Density 0.40355 4.4339 0.98342 0.89736 v Yplus 0 43.249 2.4477 0.95147 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7952e-05 43.208 0.47285 0.010605 INSTANT 0.158833145E-01 TIME STEP NUMBER 30062 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.613971222E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560748560E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123470755E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10357E+01 0.57676E+02 Friction velocity uk : 0.10357E+01 0.57676E+02 Dimensionless distance yplus : 0.20589E-01 0.43263E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14460E-01 0.12440E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60098E+03 2 0.25629E-06 0.58808E+02 0.18535E+03 c Velocity[X] 0.45921E+01 c Velocity[Y] 0.11186E+02 c Velocity[Z] 0.43031E+02 c Pressure 0.75513E-01 9 0.83691E-08 0.25901E+07 0.42357E+02 c k 0.24366E+04 1 0.93988E-06 0.89556E+05 0.15239E+04 c omega 0.81511E+09 1 0.61223E-08 0.91171E+12 0.69922E+02 c TotEner 0.24207E+06 1 0.11784E-05 0.55400E+07 0.25628E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10414E+02 0.26035E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0462e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -223.61 223.62 0.0017165 0.00068903 v Velocity[Y] -0.13041 701.9 250.47 80.935 v Velocity[Z] -19.236 350.25 24.563 1.9491 v ǁVelocityǁ 0.028161 701.9 259.8 83.678 v Pressure 52046 1.1025e+05 1.0365e+05 1.0417e+05 v k 1.1837e-08 40728 907.19 355.48 v omega 153.85 9.6778e+09 1.8456e+08 3.4141e+05 v TotEner 96587 6.2952e+05 3.4155e+05 2.4851e+05 v temperature 69.577 533.97 398.04 337.17 v Density 0.40308 4.44 0.9495 1.0904 v TurbVisc 8.816e-19 0.064126 0.010069 0.028627 v CourantNb 1.2837e-05 42.487 0.38338 0.007583 v FourierNb 4.5115e-05 217.42 1.8792 0.09056 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 69.642 533.97 403.28 422 v Boundary Density 0.40331 4.4369 0.98345 0.89737 v Yplus 0 43.263 2.4477 0.95151 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.796e-05 43.225 0.473 0.010605 INSTANT 0.158835774E-01 TIME STEP NUMBER 30063 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.615472799E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560748127E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123350184E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10357E+01 0.57685E+02 Friction velocity uk : 0.10357E+01 0.57685E+02 Dimensionless distance yplus : 0.20588E-01 0.43276E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14460E-01 0.12441E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60098E+03 2 0.25611E-06 0.58202E+02 0.18440E+03 c Velocity[X] 0.45223E+01 c Velocity[Y] 0.11180E+02 c Velocity[Z] 0.42500E+02 c Pressure 0.75517E-01 9 0.84816E-08 0.25303E+07 0.41866E+02 c k 0.24369E+04 1 0.95100E-06 0.85154E+05 0.14859E+04 c omega 0.81511E+09 1 0.61821E-08 0.97530E+12 0.72319E+02 c TotEner 0.24207E+06 1 0.11768E-05 0.53910E+07 0.25281E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10162E+02 0.25718E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.045e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -223.68 223.69 0.0017142 0.00069261 v Velocity[Y] -0.13041 701.9 250.47 80.936 v Velocity[Z] -19.236 350.44 24.57 1.9493 v ǁVelocityǁ 0.026931 701.9 259.8 83.678 v Pressure 52014 1.1025e+05 1.0365e+05 1.0417e+05 v k 1.1836e-08 40736 907.27 355.48 v omega 153.85 9.6778e+09 1.8456e+08 3.4141e+05 v TotEner 96536 6.2952e+05 3.4155e+05 2.4851e+05 v temperature 69.512 533.97 398.04 337.17 v Density 0.40285 4.4431 0.94949 1.0904 v TurbVisc 8.8153e-19 0.064126 0.010069 0.028627 v CourantNb 1.2842e-05 42.505 0.38352 0.0075832 v FourierNb 4.5114e-05 217.21 1.8784 0.090561 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 69.577 533.97 403.28 422 v Boundary Density 0.40308 4.44 0.98349 0.89738 v Yplus 0 43.276 2.4476 0.95156 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7968e-05 43.242 0.47316 0.010605 INSTANT 0.158838404E-01 TIME STEP NUMBER 30064 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.616967947E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560747782E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123230237E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10357E+01 0.57693E+02 Friction velocity uk : 0.10357E+01 0.57693E+02 Dimensionless distance yplus : 0.20588E-01 0.43290E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14459E-01 0.12442E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60098E+03 2 0.25593E-06 0.57571E+02 0.18339E+03 c Velocity[X] 0.44390E+01 c Velocity[Y] 0.11164E+02 c Velocity[Z] 0.41968E+02 c Pressure 0.75521E-01 9 0.83903E-08 0.24763E+07 0.41416E+02 c k 0.24371E+04 1 0.96375E-06 0.81674E+05 0.14551E+04 c omega 0.81512E+09 1 0.59494E-08 0.87458E+12 0.68483E+02 c TotEner 0.24207E+06 1 0.11752E-05 0.52492E+07 0.24946E+02 c temperature 0.00000E+00 0 0.00000E+00 0.99209E+01 0.25411E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0438e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -223.74 223.75 0.0017113 0.00069618 v Velocity[Y] -0.1304 701.9 250.47 80.937 v Velocity[Z] -19.235 350.62 24.578 1.9495 v ǁVelocityǁ 0.025759 701.9 259.81 83.679 v Pressure 51984 1.1025e+05 1.0364e+05 1.0417e+05 v k 1.1835e-08 40745 907.34 355.48 v omega 153.86 9.6779e+09 1.8457e+08 3.4141e+05 v TotEner 96484 6.2952e+05 3.4155e+05 2.4851e+05 v temperature 69.447 533.97 398.04 337.17 v Density 0.40263 4.4463 0.94948 1.0904 v TurbVisc 8.8146e-19 0.064126 0.010069 0.028627 v CourantNb 1.2848e-05 42.522 0.38367 0.0075834 v FourierNb 4.5112e-05 217 1.8775 0.090562 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 69.512 533.97 403.27 422 v Boundary Density 0.40285 4.4431 0.98352 0.89738 v Yplus 0 43.29 2.4476 0.9516 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7976e-05 43.258 0.47331 0.010605 INSTANT 0.158841033E-01 TIME STEP NUMBER 30065 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.618454835E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560747484E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123111523E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10356E+01 0.57702E+02 Friction velocity uk : 0.10356E+01 0.57702E+02 Dimensionless distance yplus : 0.20587E-01 0.43305E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14459E-01 0.12443E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60099E+03 2 0.25574E-06 0.56934E+02 0.18237E+03 c Velocity[X] 0.43441E+01 c Velocity[Y] 0.11158E+02 c Velocity[Z] 0.41432E+02 c Pressure 0.75525E-01 9 0.81908E-08 0.24282E+07 0.41013E+02 c k 0.24373E+04 1 0.97756E-06 0.78982E+05 0.14308E+04 c omega 0.81512E+09 1 0.62351E-08 0.83760E+12 0.67020E+02 c TotEner 0.24208E+06 1 0.11736E-05 0.51233E+07 0.24645E+02 c temperature 0.00000E+00 0 0.00000E+00 0.96988E+01 0.25125E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0427e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -223.8 223.81 0.0017081 0.00069973 v Velocity[Y] -0.1304 701.9 250.47 80.937 v Velocity[Z] -19.234 350.81 24.586 1.9497 v ǁVelocityǁ 0.024659 701.9 259.81 83.68 v Pressure 51954 1.1025e+05 1.0364e+05 1.0417e+05 v k 1.1834e-08 40754 907.42 355.48 v omega 153.86 9.6779e+09 1.8457e+08 3.4141e+05 v TotEner 96433 6.2952e+05 3.4155e+05 2.4851e+05 v temperature 69.383 533.97 398.04 337.17 v Density 0.40241 4.4495 0.94948 1.0904 v TurbVisc 8.814e-19 0.064126 0.010069 0.028627 v CourantNb 1.2854e-05 42.539 0.38381 0.0075835 v FourierNb 4.5111e-05 216.8 1.8767 0.090562 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 69.447 533.97 403.26 422 v Boundary Density 0.40263 4.4463 0.98356 0.89739 v Yplus 0 43.305 2.4476 0.95165 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7984e-05 43.274 0.47346 0.010606 INSTANT 0.158843663E-01 TIME STEP NUMBER 30066 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.619931678E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560747191E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122994641E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10356E+01 0.57710E+02 Friction velocity uk : 0.10356E+01 0.57710E+02 Dimensionless distance yplus : 0.20586E-01 0.43319E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14458E-01 0.12443E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60099E+03 2 0.25555E-06 0.56290E+02 0.18134E+03 c Velocity[X] 0.42426E+01 c Velocity[Y] 0.11155E+02 c Velocity[Z] 0.40892E+02 c Pressure 0.75529E-01 9 0.82222E-08 0.23857E+07 0.40652E+02 c k 0.24376E+04 1 0.99234E-06 0.77018E+05 0.14128E+04 c omega 0.81512E+09 1 0.63992E-08 0.85827E+12 0.67841E+02 c TotEner 0.24208E+06 1 0.11720E-05 0.50117E+07 0.24375E+02 c temperature 0.00000E+00 0 0.00000E+00 0.94959E+01 0.24861E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0416e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -223.87 223.87 0.0017046 0.00070328 v Velocity[Y] -0.13039 701.9 250.47 80.938 v Velocity[Z] -19.234 350.99 24.593 1.9498 v ǁVelocityǁ 0.023648 701.9 259.82 83.681 v Pressure 51924 1.1025e+05 1.0364e+05 1.0417e+05 v k 1.1834e-08 40764 907.49 355.48 v omega 153.87 9.6779e+09 1.8457e+08 3.4141e+05 v TotEner 96382 6.2952e+05 3.4155e+05 2.4851e+05 v temperature 69.318 533.97 398.03 337.17 v Density 0.40219 4.4528 0.94947 1.0904 v TurbVisc 8.8133e-19 0.064126 0.010069 0.028628 v CourantNb 1.2859e-05 42.556 0.38394 0.0075837 v FourierNb 4.5109e-05 216.59 1.8758 0.090563 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 69.383 533.97 403.25 422 v Boundary Density 0.40241 4.4495 0.9836 0.8974 v Yplus 0 43.319 2.4476 0.9517 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7992e-05 43.29 0.47361 0.010606 INSTANT 0.158846292E-01 TIME STEP NUMBER 30067 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.621396736E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560746863E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122880170E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10356E+01 0.57718E+02 Friction velocity uk : 0.10356E+01 0.57718E+02 Dimensionless distance yplus : 0.20585E-01 0.43334E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14458E-01 0.12444E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60099E+03 2 0.25536E-06 0.55657E+02 0.18031E+03 c Velocity[X] 0.41404E+01 c Velocity[Y] 0.11170E+02 c Velocity[Z] 0.40347E+02 c Pressure 0.75533E-01 9 0.86985E-08 0.23480E+07 0.40329E+02 c k 0.24378E+04 1 0.10081E-05 0.75647E+05 0.14001E+04 c omega 0.81512E+09 1 0.60263E-08 0.78120E+12 0.64724E+02 c TotEner 0.24208E+06 1 0.11705E-05 0.49188E+07 0.24148E+02 c temperature 0.00000E+00 0 0.00000E+00 0.93137E+01 0.24621E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0405e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -223.93 223.94 0.001701 0.00070681 v Velocity[Y] -0.13039 701.9 250.47 80.939 v Velocity[Z] -19.233 351.17 24.6 1.95 v ǁVelocityǁ 0.022747 701.9 259.82 83.682 v Pressure 51894 1.1025e+05 1.0364e+05 1.0417e+05 v k 1.1833e-08 40775 907.56 355.48 v omega 153.87 9.6779e+09 1.8457e+08 3.4142e+05 v TotEner 96331 6.2952e+05 3.4155e+05 2.4851e+05 v temperature 69.254 533.97 398.03 337.17 v Density 0.40197 4.4562 0.94946 1.0904 v TurbVisc 8.8126e-19 0.064126 0.010068 0.028628 v CourantNb 1.2865e-05 42.573 0.38408 0.0075839 v FourierNb 4.5108e-05 216.38 1.875 0.090563 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 69.318 533.97 403.24 422 v Boundary Density 0.40219 4.4528 0.98365 0.89741 v Yplus 0 43.334 2.4476 0.95175 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8e-05 43.306 0.47376 0.010606 INSTANT 0.158848922E-01 TIME STEP NUMBER 30068 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.622848317E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560746467E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122768662E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10355E+01 0.57726E+02 Friction velocity uk : 0.10355E+01 0.57726E+02 Dimensionless distance yplus : 0.20585E-01 0.43350E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14457E-01 0.12445E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60099E+03 2 0.25516E-06 0.54971E+02 0.17920E+03 c Velocity[X] 0.40422E+01 c Velocity[Y] 0.11134E+02 c Velocity[Z] 0.39796E+02 c Pressure 0.75537E-01 8 0.95258E-08 0.23146E+07 0.40042E+02 c k 0.24380E+04 1 0.10231E-05 0.74603E+05 0.13903E+04 c omega 0.81512E+09 1 0.58333E-08 0.72427E+12 0.62321E+02 c TotEner 0.24208E+06 1 0.11688E-05 0.48246E+07 0.23916E+02 c temperature 0.00000E+00 0 0.00000E+00 0.91459E+01 0.24398E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0394e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -223.99 224 0.0016973 0.00071034 v Velocity[Y] -0.13039 701.9 250.47 80.94 v Velocity[Z] -19.233 351.34 24.608 1.9502 v ǁVelocityǁ 0.021976 701.9 259.83 83.683 v Pressure 51866 1.1025e+05 1.0364e+05 1.0417e+05 v k 1.1832e-08 40786 907.62 355.48 v omega 153.88 9.6779e+09 1.8457e+08 3.4142e+05 v TotEner 96280 6.2952e+05 3.4155e+05 2.4851e+05 v temperature 69.189 533.97 398.03 337.17 v Density 0.40176 4.4596 0.94945 1.0904 v TurbVisc 8.812e-19 0.064126 0.010068 0.028628 v CourantNb 1.287e-05 42.589 0.38422 0.007584 v FourierNb 4.5107e-05 216.17 1.8742 0.090563 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 69.254 533.97 403.23 421.99 v Boundary Density 0.40197 4.4562 0.98369 0.89742 v Yplus 0 43.35 2.4476 0.9518 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8007e-05 43.322 0.47391 0.010606 INSTANT 0.158851552E-01 TIME STEP NUMBER 30069 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.624284777E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560745973E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122660644E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10355E+01 0.57734E+02 Friction velocity uk : 0.10355E+01 0.57734E+02 Dimensionless distance yplus : 0.20584E-01 0.43365E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14457E-01 0.12446E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60099E+03 2 0.25497E-06 0.54329E+02 0.17814E+03 c Velocity[X] 0.39508E+01 c Velocity[Y] 0.11136E+02 c Velocity[Z] 0.39242E+02 c Pressure 0.75541E-01 9 0.87092E-08 0.22847E+07 0.39782E+02 c k 0.24383E+04 1 0.10403E-05 0.74016E+05 0.13847E+04 c omega 0.81512E+09 1 0.54767E-08 0.65394E+12 0.59217E+02 c TotEner 0.24208E+06 1 0.11673E-05 0.47528E+07 0.23737E+02 c temperature 0.00000E+00 0 0.00000E+00 0.89996E+01 0.24202E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0383e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.05 224.06 0.0016938 0.00071387 v Velocity[Y] -0.13038 701.9 250.47 80.941 v Velocity[Z] -19.232 351.52 24.615 1.9504 v ǁVelocityǁ 0.021357 701.9 259.83 83.684 v Pressure 51837 1.1025e+05 1.0364e+05 1.0417e+05 v k 1.1831e-08 40799 907.69 355.48 v omega 153.88 9.6779e+09 1.8457e+08 3.4142e+05 v TotEner 96229 6.2952e+05 3.4155e+05 2.4851e+05 v temperature 69.125 533.97 398.03 337.17 v Density 0.40155 4.4631 0.94944 1.0904 v TurbVisc 8.8114e-19 0.064126 0.010068 0.028628 v CourantNb 1.2875e-05 42.605 0.38435 0.0075842 v FourierNb 4.5105e-05 215.97 1.8734 0.090564 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 69.189 533.97 403.23 421.99 v Boundary Density 0.40176 4.4596 0.98374 0.89743 v Yplus 0 43.365 2.4476 0.95186 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8015e-05 43.337 0.47405 0.010607 INSTANT 0.158854181E-01 TIME STEP NUMBER 30070 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.625704523E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560745366E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122556607E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10355E+01 0.57742E+02 Friction velocity uk : 0.10355E+01 0.57742E+02 Dimensionless distance yplus : 0.20584E-01 0.43381E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14457E-01 0.12447E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60100E+03 2 0.25477E-06 0.53702E+02 0.17711E+03 c Velocity[X] 0.38668E+01 c Velocity[Y] 0.11148E+02 c Velocity[Z] 0.38687E+02 c Pressure 0.75545E-01 9 0.93747E-08 0.22582E+07 0.39550E+02 c k 0.24385E+04 1 0.10582E-05 0.73684E+05 0.13815E+04 c omega 0.81512E+09 1 0.54069E-08 0.61779E+12 0.57557E+02 c TotEner 0.24208E+06 1 0.11658E-05 0.46930E+07 0.23587E+02 c temperature 0.00000E+00 0 0.00000E+00 0.88701E+01 0.24028E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0372e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.11 224.12 0.0016904 0.00071739 v Velocity[Y] -0.13038 701.9 250.48 80.942 v Velocity[Z] -19.232 351.69 24.622 1.9506 v ǁVelocityǁ 0.020913 701.9 259.84 83.685 v Pressure 51809 1.1025e+05 1.0363e+05 1.0417e+05 v k 1.183e-08 40811 907.75 355.48 v omega 153.89 9.6779e+09 1.8457e+08 3.4142e+05 v TotEner 96178 6.2952e+05 3.4155e+05 2.4851e+05 v temperature 69.062 533.97 398.03 337.17 v Density 0.40135 4.4666 0.94944 1.0904 v TurbVisc 8.8107e-19 0.064126 0.010068 0.028628 v CourantNb 1.2881e-05 42.621 0.38448 0.0075843 v FourierNb 4.5104e-05 215.76 1.8726 0.090564 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 69.125 533.97 403.22 421.99 v Boundary Density 0.40155 4.4631 0.98378 0.89744 v Yplus 0 43.381 2.4476 0.95191 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8022e-05 43.352 0.47419 0.010607 INSTANT 0.158856811E-01 TIME STEP NUMBER 30071 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.627106001E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560744622E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122457006E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10354E+01 0.57750E+02 Friction velocity uk : 0.10354E+01 0.57750E+02 Dimensionless distance yplus : 0.20583E-01 0.43397E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14456E-01 0.12448E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60100E+03 2 0.25458E-06 0.53064E+02 0.17606E+03 c Velocity[X] 0.37893E+01 c Velocity[Y] 0.11141E+02 c Velocity[Z] 0.38134E+02 c Pressure 0.75549E-01 10 0.92652E-08 0.22345E+07 0.39343E+02 c k 0.24388E+04 1 0.10743E-05 0.73486E+05 0.13796E+04 c omega 0.81512E+09 1 0.55730E-08 0.61709E+12 0.57525E+02 c TotEner 0.24208E+06 1 0.11643E-05 0.46357E+07 0.23443E+02 c temperature 0.00000E+00 0 0.00000E+00 0.87534E+01 0.23869E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0361e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.17 224.17 0.0016873 0.00072092 v Velocity[Y] -0.13037 701.9 250.48 80.943 v Velocity[Z] -19.231 351.87 24.629 1.9507 v ǁVelocityǁ 0.020663 701.9 259.85 83.686 v Pressure 51781 1.1025e+05 1.0363e+05 1.0417e+05 v k 1.183e-08 40824 907.82 355.48 v omega 153.89 9.678e+09 1.8457e+08 3.4142e+05 v TotEner 96128 6.2952e+05 3.4156e+05 2.4851e+05 v temperature 68.998 533.97 398.02 337.17 v Density 0.40114 4.4702 0.94943 1.0904 v TurbVisc 8.8101e-19 0.064126 0.010068 0.028628 v CourantNb 1.2886e-05 42.637 0.38461 0.0075845 v FourierNb 4.5103e-05 215.56 1.8718 0.090565 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 69.062 533.97 403.21 421.99 v Boundary Density 0.40135 4.4666 0.98383 0.89745 v Yplus 0 43.397 2.4476 0.95197 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.803e-05 43.367 0.47433 0.010607 INSTANT 0.158859440E-01 TIME STEP NUMBER 30072 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.628487718E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560743725E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122362258E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10354E+01 0.57757E+02 Friction velocity uk : 0.10354E+01 0.57757E+02 Dimensionless distance yplus : 0.20582E-01 0.43413E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14456E-01 0.12449E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60100E+03 2 0.25438E-06 0.52404E+02 0.17495E+03 c Velocity[X] 0.37164E+01 c Velocity[Y] 0.11103E+02 c Velocity[Z] 0.37584E+02 c Pressure 0.75553E-01 10 0.89436E-08 0.22137E+07 0.39159E+02 c k 0.24390E+04 1 0.10883E-05 0.73324E+05 0.13780E+04 c omega 0.81512E+09 1 0.57637E-08 0.66981E+12 0.59932E+02 c TotEner 0.24209E+06 1 0.11627E-05 0.45783E+07 0.23297E+02 c temperature 0.00000E+00 0 0.00000E+00 0.86477E+01 0.23724E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0351e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.22 224.23 0.0016843 0.00072443 v Velocity[Y] -0.13037 701.9 250.48 80.944 v Velocity[Z] -19.231 352.04 24.637 1.9509 v ǁVelocityǁ 0.020623 701.9 259.85 83.687 v Pressure 51751 1.1025e+05 1.0363e+05 1.0417e+05 v k 1.1829e-08 40838 907.88 355.48 v omega 153.9 9.678e+09 1.8457e+08 3.4142e+05 v TotEner 96078 6.2952e+05 3.4156e+05 2.4851e+05 v temperature 68.935 533.97 398.02 337.17 v Density 0.40095 4.4739 0.94942 1.0904 v TurbVisc 8.8096e-19 0.064125 0.010067 0.028628 v CourantNb 1.2891e-05 42.652 0.38473 0.0075846 v FourierNb 4.5101e-05 215.36 1.871 0.090565 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.998 533.97 403.21 421.99 v Boundary Density 0.40114 4.4702 0.98388 0.89746 v Yplus 0 43.413 2.4476 0.95202 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8037e-05 43.382 0.47447 0.010607 INSTANT 0.158862070E-01 TIME STEP NUMBER 30073 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.629848231E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560742669E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122272732E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10354E+01 0.57765E+02 Friction velocity uk : 0.10354E+01 0.57765E+02 Dimensionless distance yplus : 0.20582E-01 0.43430E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14455E-01 0.12450E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60100E+03 2 0.25419E-06 0.51780E+02 0.17391E+03 c Velocity[X] 0.36467E+01 c Velocity[Y] 0.11090E+02 c Velocity[Z] 0.37043E+02 c Pressure 0.75557E-01 9 0.87877E-08 0.21950E+07 0.38994E+02 c k 0.24393E+04 1 0.11038E-05 0.73299E+05 0.13776E+04 c omega 0.81512E+09 1 0.52808E-08 0.57940E+12 0.55740E+02 c TotEner 0.24209E+06 1 0.11612E-05 0.45332E+07 0.23182E+02 c temperature 0.00000E+00 0 0.00000E+00 0.85543E+01 0.23596E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0341e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.28 224.29 0.0016812 0.00072793 v Velocity[Y] -0.13036 701.9 250.48 80.945 v Velocity[Z] -19.23 352.21 24.644 1.9511 v ǁVelocityǁ 0.020804 701.9 259.86 83.688 v Pressure 51721 1.1025e+05 1.0363e+05 1.0417e+05 v k 1.1828e-08 40852 907.94 355.48 v omega 153.9 9.678e+09 1.8457e+08 3.4142e+05 v TotEner 96029 6.2952e+05 3.4156e+05 2.4851e+05 v temperature 68.873 533.97 398.02 337.17 v Density 0.40075 4.4776 0.94942 1.0904 v TurbVisc 8.809e-19 0.064125 0.010067 0.028629 v CourantNb 1.2896e-05 42.667 0.38486 0.0075848 v FourierNb 4.51e-05 215.16 1.8702 0.090565 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.935 533.97 403.2 421.99 v Boundary Density 0.40095 4.4739 0.98394 0.89748 v Yplus 0 43.43 2.4476 0.95208 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8044e-05 43.397 0.47461 0.010607 INSTANT 0.158864700E-01 TIME STEP NUMBER 30074 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.631186145E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560741428E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122188759E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10354E+01 0.57772E+02 Friction velocity uk : 0.10354E+01 0.57772E+02 Dimensionless distance yplus : 0.20581E-01 0.43447E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14455E-01 0.12451E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60100E+03 2 0.25399E-06 0.51164E+02 0.17287E+03 c Velocity[X] 0.35790E+01 c Velocity[Y] 0.11073E+02 c Velocity[Z] 0.36512E+02 c Pressure 0.75561E-01 9 0.86839E-08 0.21783E+07 0.38845E+02 c k 0.24395E+04 1 0.11196E-05 0.73334E+05 0.13779E+04 c omega 0.81512E+09 1 0.54097E-08 0.60726E+12 0.57065E+02 c TotEner 0.24209E+06 1 0.11597E-05 0.44899E+07 0.23071E+02 c temperature 0.00000E+00 0 0.00000E+00 0.84678E+01 0.23476E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0331e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.34 224.34 0.0016784 0.00073143 v Velocity[Y] -0.13036 701.9 250.48 80.946 v Velocity[Z] -19.23 352.37 24.65 1.9513 v ǁVelocityǁ 0.021208 701.9 259.86 83.689 v Pressure 51692 1.1025e+05 1.0363e+05 1.0417e+05 v k 1.1827e-08 40867 908 355.47 v omega 153.91 9.678e+09 1.8457e+08 3.4142e+05 v TotEner 95979 6.2952e+05 3.4156e+05 2.4851e+05 v temperature 68.81 533.97 398.02 337.17 v Density 0.40056 4.4814 0.94941 1.0904 v TurbVisc 8.8084e-19 0.064125 0.010067 0.028629 v CourantNb 1.2901e-05 42.682 0.38498 0.007585 v FourierNb 4.5099e-05 214.96 1.8695 0.090566 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.873 533.97 403.19 421.99 v Boundary Density 0.40075 4.4776 0.98399 0.89749 v Yplus 0 43.447 2.4476 0.95214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8051e-05 43.411 0.47474 0.010608 INSTANT 0.158867329E-01 TIME STEP NUMBER 30075 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.632500116E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560739984E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122110619E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10353E+01 0.57779E+02 Friction velocity uk : 0.10353E+01 0.57779E+02 Dimensionless distance yplus : 0.20580E-01 0.43464E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14454E-01 0.12451E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60100E+03 2 0.25380E-06 0.50577E+02 0.17187E+03 c Velocity[X] 0.35129E+01 c Velocity[Y] 0.11069E+02 c Velocity[Z] 0.35995E+02 c Pressure 0.75565E-01 9 0.87127E-08 0.21634E+07 0.38711E+02 c k 0.24398E+04 1 0.11354E-05 0.73409E+05 0.13785E+04 c omega 0.81512E+09 1 0.53176E-08 0.59072E+12 0.56282E+02 c TotEner 0.24209E+06 1 0.11583E-05 0.44523E+07 0.22974E+02 c temperature 0.00000E+00 0 0.00000E+00 0.83884E+01 0.23366E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0321e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.39 224.4 0.0016759 0.00073494 v Velocity[Y] -0.13036 701.9 250.48 80.947 v Velocity[Z] -19.229 352.54 24.657 1.9514 v ǁVelocityǁ 0.021831 701.9 259.87 83.689 v Pressure 51664 1.1025e+05 1.0363e+05 1.0417e+05 v k 1.1827e-08 40882 908.06 355.47 v omega 153.91 9.678e+09 1.8457e+08 3.4142e+05 v TotEner 95930 6.2952e+05 3.4156e+05 2.4851e+05 v temperature 68.748 533.97 398.02 337.17 v Density 0.40037 4.4852 0.9494 1.0904 v TurbVisc 8.8078e-19 0.064125 0.010067 0.028629 v CourantNb 1.2906e-05 42.697 0.3851 0.0075851 v FourierNb 4.5097e-05 214.77 1.8687 0.090566 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.81 533.97 403.19 421.99 v Boundary Density 0.40056 4.4814 0.98404 0.8975 v Yplus 0 43.464 2.4476 0.9522 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8058e-05 43.426 0.47487 0.010608 INSTANT 0.158869959E-01 TIME STEP NUMBER 30076 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.633788856E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560738358E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122038549E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10353E+01 0.57786E+02 Friction velocity uk : 0.10353E+01 0.57786E+02 Dimensionless distance yplus : 0.20580E-01 0.43482E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14454E-01 0.12452E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60101E+03 2 0.25361E-06 0.50009E+02 0.17091E+03 c Velocity[X] 0.34487E+01 c Velocity[Y] 0.11067E+02 c Velocity[Z] 0.35494E+02 c Pressure 0.75569E-01 5 0.98009E-08 0.21497E+07 0.38589E+02 c k 0.24400E+04 1 0.11502E-05 0.73471E+05 0.13790E+04 c omega 0.81512E+09 1 0.52445E-08 0.55566E+12 0.54586E+02 c TotEner 0.24209E+06 1 0.11569E-05 0.44164E+07 0.22882E+02 c temperature 0.00000E+00 0 0.00000E+00 0.83128E+01 0.23260E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0311e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.45 224.45 0.0016738 0.00073846 v Velocity[Y] -0.13035 701.9 250.48 80.948 v Velocity[Z] -19.228 352.7 24.664 1.9516 v ǁVelocityǁ 0.021903 701.9 259.87 83.69 v Pressure 51635 1.1025e+05 1.0363e+05 1.0417e+05 v k 1.1826e-08 40897 908.12 355.47 v omega 153.92 9.678e+09 1.8457e+08 3.4142e+05 v TotEner 95882 6.2952e+05 3.4156e+05 2.4851e+05 v temperature 68.686 533.97 398.01 337.17 v Density 0.40018 4.4891 0.9494 1.0904 v TurbVisc 8.8073e-19 0.064125 0.010067 0.028629 v CourantNb 1.2911e-05 42.711 0.38522 0.0075853 v FourierNb 4.5096e-05 214.57 1.868 0.090566 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.748 533.97 403.18 421.98 v Boundary Density 0.40037 4.4852 0.9841 0.89751 v Yplus 0 43.482 2.4476 0.95226 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8065e-05 43.44 0.475 0.010608 INSTANT 0.158872589E-01 TIME STEP NUMBER 30077 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.635051130E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560736582E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121972738E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10353E+01 0.57793E+02 Friction velocity uk : 0.10353E+01 0.57793E+02 Dimensionless distance yplus : 0.20580E-01 0.43500E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14454E-01 0.12453E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60101E+03 2 0.25342E-06 0.49455E+02 0.16995E+03 c Velocity[X] 0.33868E+01 c Velocity[Y] 0.11056E+02 c Velocity[Z] 0.35012E+02 c Pressure 0.75573E-01 5 0.93335E-08 0.21368E+07 0.38473E+02 c k 0.24403E+04 1 0.11641E-05 0.73530E+05 0.13794E+04 c omega 0.81512E+09 1 0.50493E-08 0.52149E+12 0.52881E+02 c TotEner 0.24209E+06 1 0.11556E-05 0.43788E+07 0.22784E+02 c temperature 0.00000E+00 0 0.00000E+00 0.82387E+01 0.23156E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0301e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.5 224.51 0.0016721 0.00074197 v Velocity[Y] -0.13035 701.9 250.48 80.949 v Velocity[Z] -19.228 352.87 24.671 1.9518 v ǁVelocityǁ 0.020988 701.9 259.88 83.691 v Pressure 51608 1.1025e+05 1.0362e+05 1.0417e+05 v k 1.1825e-08 40912 908.17 355.47 v omega 153.92 9.678e+09 1.8457e+08 3.4142e+05 v TotEner 95834 6.2952e+05 3.4156e+05 2.4851e+05 v temperature 68.625 533.97 398.01 337.17 v Density 0.4 4.493 0.94939 1.0904 v TurbVisc 8.8065e-19 0.064125 0.010067 0.028629 v CourantNb 1.2916e-05 42.725 0.38534 0.0075854 v FourierNb 4.5095e-05 214.38 1.8672 0.090567 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.686 533.97 403.17 421.98 v Boundary Density 0.40018 4.4891 0.98416 0.89752 v Yplus 0 43.5 2.4476 0.95231 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8072e-05 43.454 0.47513 0.010608 INSTANT 0.158875218E-01 TIME STEP NUMBER 30078 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.636285754E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560734665E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121913327E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10353E+01 0.57800E+02 Friction velocity uk : 0.10353E+01 0.57800E+02 Dimensionless distance yplus : 0.20579E-01 0.43518E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14454E-01 0.12454E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60101E+03 2 0.25323E-06 0.48926E+02 0.16904E+03 c Velocity[X] 0.33277E+01 c Velocity[Y] 0.11048E+02 c Velocity[Z] 0.34551E+02 c Pressure 0.75577E-01 5 0.88311E-08 0.21245E+07 0.38362E+02 c k 0.24405E+04 1 0.11778E-05 0.73611E+05 0.13801E+04 c omega 0.81512E+09 1 0.48943E-08 0.48163E+12 0.50820E+02 c TotEner 0.24209E+06 1 0.11543E-05 0.43427E+07 0.22690E+02 c temperature 0.00000E+00 0 0.00000E+00 0.81665E+01 0.23055E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0292e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.55 224.56 0.0016707 0.00074549 v Velocity[Y] -0.13034 701.9 250.48 80.95 v Velocity[Z] -19.227 353.03 24.678 1.952 v ǁVelocityǁ 0.020278 701.9 259.88 83.692 v Pressure 51581 1.1025e+05 1.0362e+05 1.0417e+05 v k 1.1824e-08 40928 908.23 355.47 v omega 153.93 9.678e+09 1.8457e+08 3.4142e+05 v TotEner 95786 6.2952e+05 3.4156e+05 2.4851e+05 v temperature 68.564 533.97 398.01 337.17 v Density 0.39982 4.497 0.94938 1.0904 v TurbVisc 8.8058e-19 0.064125 0.010066 0.028629 v CourantNb 1.2921e-05 42.739 0.38546 0.0075856 v FourierNb 4.5094e-05 214.19 1.8665 0.090567 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.625 533.97 403.17 421.98 v Boundary Density 0.4 4.493 0.98421 0.89753 v Yplus 0 43.518 2.4476 0.95237 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8079e-05 43.467 0.47526 0.010608 INSTANT 0.158877848E-01 TIME STEP NUMBER 30079 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.637491600E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560732621E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121860416E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10352E+01 0.57807E+02 Friction velocity uk : 0.10352E+01 0.57807E+02 Dimensionless distance yplus : 0.20579E-01 0.43536E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14453E-01 0.12455E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60101E+03 2 0.25305E-06 0.48427E+02 0.16818E+03 c Velocity[X] 0.32714E+01 c Velocity[Y] 0.11044E+02 c Velocity[Z] 0.34112E+02 c Pressure 0.75581E-01 5 0.96167E-08 0.21123E+07 0.38252E+02 c k 0.24408E+04 1 0.11906E-05 0.73710E+05 0.13809E+04 c omega 0.81512E+09 1 0.48693E-08 0.49981E+12 0.51770E+02 c TotEner 0.24210E+06 1 0.11530E-05 0.43079E+07 0.22599E+02 c temperature 0.00000E+00 0 0.00000E+00 0.80958E+01 0.22955E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0282e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.6 224.61 0.0016697 0.000749 v Velocity[Y] -0.13034 701.9 250.48 80.951 v Velocity[Z] -19.227 353.19 24.684 1.9522 v ǁVelocityǁ 0.019805 701.9 259.89 83.693 v Pressure 51554 1.1025e+05 1.0362e+05 1.0417e+05 v k 1.1823e-08 40945 908.29 355.47 v omega 153.93 9.678e+09 1.8457e+08 3.4142e+05 v TotEner 95738 6.2952e+05 3.4156e+05 2.4851e+05 v temperature 68.503 533.97 398.01 337.17 v Density 0.39964 4.501 0.94938 1.0904 v TurbVisc 8.8051e-19 0.064125 0.010066 0.02863 v CourantNb 1.2926e-05 42.753 0.38557 0.0075857 v FourierNb 4.5093e-05 214 1.8658 0.090568 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.564 533.97 403.16 421.98 v Boundary Density 0.39982 4.497 0.98427 0.89754 v Yplus 0 43.536 2.4476 0.95243 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8086e-05 43.481 0.47539 0.010609 INSTANT 0.158880478E-01 TIME STEP NUMBER 30080 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.638667593E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560730478E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121814056E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10352E+01 0.57814E+02 Friction velocity uk : 0.10352E+01 0.57814E+02 Dimensionless distance yplus : 0.20578E-01 0.43555E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14453E-01 0.12456E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60101E+03 2 0.25286E-06 0.47956E+02 0.16735E+03 c Velocity[X] 0.32177E+01 c Velocity[Y] 0.11043E+02 c Velocity[Z] 0.33696E+02 c Pressure 0.75585E-01 5 0.94846E-08 0.21002E+07 0.38142E+02 c k 0.24411E+04 1 0.12026E-05 0.73828E+05 0.13819E+04 c omega 0.81512E+09 1 0.52095E-08 0.52886E+12 0.53253E+02 c TotEner 0.24210E+06 1 0.11518E-05 0.42744E+07 0.22511E+02 c temperature 0.00000E+00 0 0.00000E+00 0.80267E+01 0.22856E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0273e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.65 224.66 0.0016691 0.00075252 v Velocity[Y] -0.13034 701.9 250.48 80.952 v Velocity[Z] -19.226 353.35 24.691 1.9523 v ǁVelocityǁ 0.019595 701.9 259.89 83.694 v Pressure 51528 1.1025e+05 1.0362e+05 1.0417e+05 v k 1.1822e-08 40961 908.34 355.47 v omega 153.94 9.678e+09 1.8457e+08 3.4142e+05 v TotEner 95691 6.2952e+05 3.4156e+05 2.4851e+05 v temperature 68.442 533.97 398.01 337.17 v Density 0.39947 4.5051 0.94937 1.0904 v TurbVisc 8.8045e-19 0.064125 0.010066 0.02863 v CourantNb 1.2931e-05 42.767 0.38569 0.0075859 v FourierNb 4.5092e-05 213.82 1.8651 0.090568 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.503 533.97 403.16 421.98 v Boundary Density 0.39964 4.501 0.98433 0.89756 v Yplus 0 43.555 2.4476 0.95249 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8092e-05 43.494 0.47551 0.010609 INSTANT 0.158883108E-01 TIME STEP NUMBER 30081 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.639812714E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560728271E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121774260E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10352E+01 0.57820E+02 Friction velocity uk : 0.10352E+01 0.57820E+02 Dimensionless distance yplus : 0.20578E-01 0.43574E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14452E-01 0.12457E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60102E+03 2 0.25268E-06 0.47508E+02 0.16657E+03 c Velocity[X] 0.31660E+01 c Velocity[Y] 0.11040E+02 c Velocity[Z] 0.33303E+02 c Pressure 0.75589E-01 5 0.94365E-08 0.20880E+07 0.38032E+02 c k 0.24413E+04 1 0.12133E-05 0.73939E+05 0.13829E+04 c omega 0.81512E+09 1 0.47440E-08 0.44895E+12 0.49065E+02 c TotEner 0.24210E+06 1 0.11506E-05 0.42419E+07 0.22425E+02 c temperature 0.00000E+00 0 0.00000E+00 0.79596E+01 0.22761E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0264e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.71 224.71 0.0016689 0.00075604 v Velocity[Y] -0.13033 701.9 250.48 80.953 v Velocity[Z] -19.226 353.51 24.697 1.9525 v ǁVelocityǁ 0.019669 701.9 259.9 83.695 v Pressure 51502 1.1025e+05 1.0362e+05 1.0417e+05 v k 1.1822e-08 40978 908.4 355.47 v omega 153.94 9.678e+09 1.8458e+08 3.4142e+05 v TotEner 95644 6.2952e+05 3.4156e+05 2.4851e+05 v temperature 68.381 533.97 398.01 337.17 v Density 0.39929 4.5092 0.94937 1.0904 v TurbVisc 8.8039e-19 0.064124 0.010066 0.02863 v CourantNb 1.2936e-05 42.78 0.3858 0.007586 v FourierNb 4.5091e-05 213.63 1.8644 0.090568 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.442 533.97 403.15 421.98 v Boundary Density 0.39947 4.5051 0.9844 0.89757 v Yplus 0 43.574 2.4476 0.95255 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8099e-05 43.507 0.47563 0.010609 INSTANT 0.158885737E-01 TIME STEP NUMBER 30082 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.640925997E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560726032E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121740997E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10352E+01 0.57827E+02 Friction velocity uk : 0.10352E+01 0.57827E+02 Dimensionless distance yplus : 0.20577E-01 0.43592E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14452E-01 0.12458E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60102E+03 2 0.25250E-06 0.47085E+02 0.16582E+03 c Velocity[X] 0.31157E+01 c Velocity[Y] 0.11036E+02 c Velocity[Z] 0.32933E+02 c Pressure 0.75593E-01 5 0.94253E-08 0.20755E+07 0.37917E+02 c k 0.24416E+04 1 0.12236E-05 0.74099E+05 0.13843E+04 c omega 0.81512E+09 1 0.50089E-08 0.55435E+12 0.54521E+02 c TotEner 0.24210E+06 1 0.11494E-05 0.42106E+07 0.22342E+02 c temperature 0.00000E+00 0 0.00000E+00 0.78951E+01 0.22668E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0255e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.76 224.76 0.0016691 0.00075956 v Velocity[Y] -0.13033 701.9 250.48 80.954 v Velocity[Z] -19.225 353.66 24.704 1.9527 v ǁVelocityǁ 0.020032 701.9 259.9 83.696 v Pressure 51476 1.1025e+05 1.0362e+05 1.0417e+05 v k 1.1821e-08 40995 908.45 355.47 v omega 153.95 9.678e+09 1.8458e+08 3.4142e+05 v TotEner 95597 6.2952e+05 3.4156e+05 2.4851e+05 v temperature 68.321 533.97 398 337.17 v Density 0.39913 4.5133 0.94936 1.0904 v TurbVisc 8.8034e-19 0.064124 0.010066 0.02863 v CourantNb 1.2941e-05 42.793 0.38591 0.0075862 v FourierNb 4.509e-05 213.45 1.8637 0.090569 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.381 533.97 403.15 421.98 v Boundary Density 0.39929 4.5092 0.98446 0.89758 v Yplus 0 43.592 2.4477 0.95261 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8106e-05 43.52 0.47575 0.010609 INSTANT 0.158888367E-01 TIME STEP NUMBER 30083 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.642006532E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560723800E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121714201E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10351E+01 0.57833E+02 Friction velocity uk : 0.10351E+01 0.57833E+02 Dimensionless distance yplus : 0.20577E-01 0.43612E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14452E-01 0.12460E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60102E+03 2 0.25232E-06 0.46701E+02 0.16515E+03 c Velocity[X] 0.30662E+01 c Velocity[Y] 0.11048E+02 c Velocity[Z] 0.32587E+02 c Pressure 0.75597E-01 5 0.92891E-08 0.20629E+07 0.37802E+02 c k 0.24418E+04 1 0.12331E-05 0.74308E+05 0.13861E+04 c omega 0.81512E+09 1 0.50821E-08 0.65502E+12 0.59266E+02 c TotEner 0.24210E+06 1 0.11483E-05 0.41864E+07 0.22278E+02 c temperature 0.00000E+00 0 0.00000E+00 0.78363E+01 0.22584E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0246e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.8 224.81 0.0016697 0.00076308 v Velocity[Y] -0.13032 701.9 250.48 80.955 v Velocity[Z] -19.225 353.82 24.71 1.9529 v ǁVelocityǁ 0.020681 701.9 259.91 83.697 v Pressure 51451 1.1025e+05 1.0362e+05 1.0417e+05 v k 1.182e-08 41012 908.5 355.47 v omega 153.95 9.678e+09 1.8458e+08 3.4142e+05 v TotEner 95551 6.2952e+05 3.4156e+05 2.4851e+05 v temperature 68.261 533.97 398 337.17 v Density 0.39896 4.5174 0.94936 1.0904 v TurbVisc 8.8028e-19 0.064124 0.010066 0.02863 v CourantNb 1.2945e-05 42.806 0.38602 0.0075863 v FourierNb 4.5088e-05 213.27 1.863 0.090569 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.321 533.97 403.14 421.98 v Boundary Density 0.39913 4.5133 0.98452 0.89759 v Yplus 0 43.612 2.4477 0.95267 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8112e-05 43.533 0.47587 0.01061 INSTANT 0.158890997E-01 TIME STEP NUMBER 30084 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.643053466E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560721613E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121693767E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10351E+01 0.57840E+02 Friction velocity uk : 0.10351E+01 0.57840E+02 Dimensionless distance yplus : 0.20576E-01 0.43631E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14451E-01 0.12461E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60102E+03 2 0.25215E-06 0.46330E+02 0.16449E+03 c Velocity[X] 0.30169E+01 c Velocity[Y] 0.11048E+02 c Velocity[Z] 0.32264E+02 c Pressure 0.75601E-01 5 0.95449E-08 0.20498E+07 0.37682E+02 c k 0.24421E+04 1 0.12419E-05 0.74545E+05 0.13882E+04 c omega 0.81512E+09 1 0.54502E-08 0.67426E+12 0.60130E+02 c TotEner 0.24210E+06 1 0.11472E-05 0.41619E+07 0.22212E+02 c temperature 0.00000E+00 0 0.00000E+00 0.77808E+01 0.22504E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0237e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.85 224.86 0.0016707 0.00076661 v Velocity[Y] -0.13032 701.9 250.49 80.956 v Velocity[Z] -19.224 353.97 24.716 1.953 v ǁVelocityǁ 0.021599 701.9 259.91 83.698 v Pressure 51426 1.1025e+05 1.0362e+05 1.0417e+05 v k 1.1819e-08 41029 908.55 355.47 v omega 153.96 9.6781e+09 1.8458e+08 3.4142e+05 v TotEner 95505 6.2952e+05 3.4156e+05 2.4851e+05 v temperature 68.2 533.96 398 337.17 v Density 0.39879 4.5216 0.94935 1.0904 v TurbVisc 8.8023e-19 0.064124 0.010065 0.02863 v CourantNb 1.295e-05 42.819 0.38612 0.0075865 v FourierNb 4.5087e-05 213.1 1.8624 0.09057 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.261 533.97 403.14 421.98 v Boundary Density 0.39896 4.5174 0.98459 0.8976 v Yplus 0 43.631 2.4477 0.95273 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8119e-05 43.545 0.47599 0.01061 INSTANT 0.158893627E-01 TIME STEP NUMBER 30085 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.644065998E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560719514E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121679561E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10351E+01 0.57846E+02 Friction velocity uk : 0.10351E+01 0.57846E+02 Dimensionless distance yplus : 0.20576E-01 0.43650E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14451E-01 0.12462E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60102E+03 2 0.25198E-06 0.45974E+02 0.16385E+03 c Velocity[X] 0.29677E+01 c Velocity[Y] 0.11043E+02 c Velocity[Z] 0.31963E+02 c Pressure 0.75605E-01 5 0.94323E-08 0.20363E+07 0.37558E+02 c k 0.24423E+04 1 0.12490E-05 0.74717E+05 0.13897E+04 c omega 0.81512E+09 1 0.57171E-08 0.63751E+12 0.58468E+02 c TotEner 0.24210E+06 1 0.11462E-05 0.41392E+07 0.22151E+02 c temperature 0.00000E+00 0 0.00000E+00 0.77299E+01 0.22430E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0229e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.9 224.9 0.0016721 0.00077015 v Velocity[Y] -0.13031 701.9 250.49 80.956 v Velocity[Z] -19.224 354.13 24.722 1.9532 v ǁVelocityǁ 0.022763 701.9 259.92 83.699 v Pressure 51402 1.1025e+05 1.0361e+05 1.0417e+05 v k 1.1819e-08 41047 908.6 355.47 v omega 153.96 9.6781e+09 1.8458e+08 3.4142e+05 v TotEner 95458 6.2951e+05 3.4157e+05 2.4851e+05 v temperature 68.14 533.96 398 337.17 v Density 0.39863 4.5258 0.94935 1.0904 v TurbVisc 8.8018e-19 0.064124 0.010065 0.028631 v CourantNb 1.2955e-05 42.832 0.38623 0.0075866 v FourierNb 4.5087e-05 212.92 1.8617 0.09057 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.2 533.96 403.13 421.97 v Boundary Density 0.39879 4.5216 0.98465 0.89762 v Yplus 0 43.65 2.4477 0.95279 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8126e-05 43.558 0.4761 0.01061 INSTANT 0.158896256E-01 TIME STEP NUMBER 30086 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.645043377E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560717551E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121671416E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10351E+01 0.57852E+02 Friction velocity uk : 0.10351E+01 0.57852E+02 Dimensionless distance yplus : 0.20575E-01 0.43670E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14451E-01 0.12463E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60102E+03 2 0.25180E-06 0.45651E+02 0.16327E+03 c Velocity[X] 0.29185E+01 c Velocity[Y] 0.11049E+02 c Velocity[Z] 0.31683E+02 c Pressure 0.75609E-01 5 0.92460E-08 0.20227E+07 0.37431E+02 c k 0.24426E+04 1 0.12557E-05 0.74971E+05 0.13920E+04 c omega 0.81513E+09 1 0.60260E-08 0.68158E+12 0.60455E+02 c TotEner 0.24211E+06 1 0.11452E-05 0.41241E+07 0.22111E+02 c temperature 0.00000E+00 0 0.00000E+00 0.76866E+01 0.22367E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.022e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.95 224.95 0.0016739 0.00077368 v Velocity[Y] -0.13031 701.9 250.49 80.957 v Velocity[Z] -19.223 354.28 24.729 1.9534 v ǁVelocityǁ 0.024145 701.9 259.92 83.699 v Pressure 51378 1.1025e+05 1.0361e+05 1.0417e+05 v k 1.1818e-08 41064 908.65 355.47 v omega 153.97 9.6781e+09 1.8458e+08 3.4142e+05 v TotEner 95412 6.2951e+05 3.4157e+05 2.4852e+05 v temperature 68.079 533.96 398 337.17 v Density 0.39847 4.53 0.94934 1.0904 v TurbVisc 8.8013e-19 0.064124 0.010065 0.028631 v CourantNb 1.296e-05 42.844 0.38633 0.0075868 v FourierNb 4.5086e-05 212.75 1.8611 0.090571 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.14 533.96 403.13 421.97 v Boundary Density 0.39863 4.5258 0.98472 0.89763 v Yplus 0 43.67 2.4477 0.95286 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8132e-05 43.57 0.47621 0.01061 INSTANT 0.158898886E-01 TIME STEP NUMBER 30087 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.645984914E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560715763E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121669139E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10350E+01 0.57858E+02 Friction velocity uk : 0.10350E+01 0.57858E+02 Dimensionless distance yplus : 0.20575E-01 0.43690E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14450E-01 0.12464E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60103E+03 2 0.25164E-06 0.45337E+02 0.16271E+03 c Velocity[X] 0.28695E+01 c Velocity[Y] 0.11044E+02 c Velocity[Z] 0.31424E+02 c Pressure 0.75613E-01 5 0.94087E-08 0.20089E+07 0.37304E+02 c k 0.24429E+04 1 0.12615E-05 0.75210E+05 0.13941E+04 c omega 0.81513E+09 1 0.58707E-08 0.59842E+12 0.56647E+02 c TotEner 0.24211E+06 1 0.11443E-05 0.41099E+07 0.22073E+02 c temperature 0.00000E+00 0 0.00000E+00 0.76493E+01 0.22313E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0212e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -224.99 225 0.0016757 0.00077721 v Velocity[Y] -0.13031 701.9 250.49 80.958 v Velocity[Z] -19.222 354.43 24.735 1.9536 v ǁVelocityǁ 0.02572 701.9 259.92 83.7 v Pressure 51354 1.1025e+05 1.0361e+05 1.0417e+05 v k 1.1818e-08 41082 908.69 355.46 v omega 153.97 9.6781e+09 1.8458e+08 3.4142e+05 v TotEner 95366 6.2951e+05 3.4157e+05 2.4852e+05 v temperature 68.019 533.96 398 337.18 v Density 0.39832 4.5342 0.94934 1.0904 v TurbVisc 8.8008e-19 0.064124 0.010065 0.028631 v CourantNb 1.2964e-05 42.857 0.38644 0.0075869 v FourierNb 4.5085e-05 212.58 1.8605 0.090571 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.079 533.96 403.12 421.97 v Boundary Density 0.39847 4.53 0.98478 0.89764 v Yplus 0 43.69 2.4477 0.95292 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8139e-05 43.582 0.47633 0.01061 INSTANT 0.158901516E-01 TIME STEP NUMBER 30088 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.646889980E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560714184E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121672515E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10350E+01 0.57864E+02 Friction velocity uk : 0.10350E+01 0.57864E+02 Dimensionless distance yplus : 0.20574E-01 0.43709E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14450E-01 0.12465E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60103E+03 2 0.25147E-06 0.45067E+02 0.16222E+03 c Velocity[X] 0.28211E+01 c Velocity[Y] 0.11063E+02 c Velocity[Z] 0.31183E+02 c Pressure 0.75617E-01 5 0.95314E-08 0.19945E+07 0.37170E+02 c k 0.24431E+04 1 0.12673E-05 0.75507E+05 0.13968E+04 c omega 0.81513E+09 1 0.57746E-08 0.59764E+12 0.56610E+02 c TotEner 0.24211E+06 1 0.11434E-05 0.41056E+07 0.22061E+02 c temperature 0.00000E+00 0 0.00000E+00 0.76197E+01 0.22269E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0204e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.04 225.04 0.0016775 0.00078072 v Velocity[Y] -0.1303 701.9 250.49 80.959 v Velocity[Z] -19.222 354.58 24.741 1.9538 v ǁVelocityǁ 0.027462 701.9 259.93 83.701 v Pressure 51331 1.1025e+05 1.0361e+05 1.0417e+05 v k 1.1817e-08 41100 908.74 355.46 v omega 153.98 9.6781e+09 1.8458e+08 3.4142e+05 v TotEner 95321 6.2951e+05 3.4157e+05 2.4852e+05 v temperature 67.958 533.96 397.99 337.18 v Density 0.39816 4.5385 0.94933 1.0904 v TurbVisc 8.8003e-19 0.064124 0.010065 0.028631 v CourantNb 1.2969e-05 42.869 0.38654 0.0075871 v FourierNb 4.5084e-05 212.42 1.8598 0.090571 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 68.019 533.96 403.12 421.97 v Boundary Density 0.39832 4.5342 0.98485 0.89765 v Yplus 0 43.709 2.4477 0.95298 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8145e-05 43.594 0.47644 0.010611 INSTANT 0.158904146E-01 TIME STEP NUMBER 30089 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.647757996E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560712843E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121681305E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10350E+01 0.57870E+02 Friction velocity uk : 0.10350E+01 0.57870E+02 Dimensionless distance yplus : 0.20574E-01 0.43729E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14450E-01 0.12466E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60103E+03 2 0.25130E-06 0.44764E+02 0.16168E+03 c Velocity[X] 0.27735E+01 c Velocity[Y] 0.11031E+02 c Velocity[Z] 0.30960E+02 c Pressure 0.75621E-01 9 0.86448E-08 0.19804E+07 0.37038E+02 c k 0.24434E+04 1 0.12700E-05 0.75598E+05 0.13975E+04 c omega 0.81513E+09 1 0.51270E-08 0.47291E+12 0.50357E+02 c TotEner 0.24211E+06 1 0.11424E-05 0.40915E+07 0.22023E+02 c temperature 0.00000E+00 0 0.00000E+00 0.75924E+01 0.22229E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0196e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.08 225.09 0.0016794 0.00078423 v Velocity[Y] -0.1303 701.9 250.49 80.96 v Velocity[Z] -19.221 354.73 24.747 1.9539 v ǁVelocityǁ 0.029349 701.9 259.93 83.702 v Pressure 51308 1.1025e+05 1.0361e+05 1.0417e+05 v k 1.1816e-08 41118 908.78 355.46 v omega 153.98 9.6781e+09 1.8458e+08 3.4142e+05 v TotEner 95275 6.2951e+05 3.4157e+05 2.4852e+05 v temperature 67.897 533.96 397.99 337.18 v Density 0.39801 4.5427 0.94933 1.0904 v TurbVisc 8.7998e-19 0.064124 0.010065 0.028631 v CourantNb 1.2974e-05 42.881 0.38664 0.0075872 v FourierNb 4.5083e-05 212.25 1.8592 0.090572 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.958 533.96 403.11 421.97 v Boundary Density 0.39816 4.5385 0.98492 0.89767 v Yplus 0 43.729 2.4477 0.95304 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8152e-05 43.606 0.47654 0.010611 INSTANT 0.158906776E-01 TIME STEP NUMBER 30090 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.648588443E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560711770E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121695253E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10350E+01 0.57875E+02 Friction velocity uk : 0.10350E+01 0.57875E+02 Dimensionless distance yplus : 0.20573E-01 0.43749E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14449E-01 0.12467E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60103E+03 2 0.25114E-06 0.44522E+02 0.16124E+03 c Velocity[X] 0.27268E+01 c Velocity[Y] 0.11042E+02 c Velocity[Z] 0.30753E+02 c Pressure 0.75625E-01 5 0.93755E-08 0.19657E+07 0.36900E+02 c k 0.24436E+04 1 0.12740E-05 0.75811E+05 0.13994E+04 c omega 0.81513E+09 1 0.52083E-08 0.47614E+12 0.50529E+02 c TotEner 0.24211E+06 1 0.11416E-05 0.40922E+07 0.22025E+02 c temperature 0.00000E+00 0 0.00000E+00 0.75746E+01 0.22203E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0188e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.13 225.13 0.0016813 0.00078775 v Velocity[Y] -0.13029 701.9 250.49 80.961 v Velocity[Z] -19.221 354.88 24.753 1.9541 v ǁVelocityǁ 0.031362 701.9 259.94 83.703 v Pressure 51285 1.1025e+05 1.0361e+05 1.0417e+05 v k 1.1816e-08 41136 908.83 355.46 v omega 153.98 9.6781e+09 1.8458e+08 3.4142e+05 v TotEner 95229 6.2951e+05 3.4157e+05 2.4852e+05 v temperature 67.837 533.96 397.99 337.18 v Density 0.39786 4.547 0.94932 1.0904 v TurbVisc 8.7995e-19 0.064124 0.010065 0.028631 v CourantNb 1.2978e-05 42.892 0.38674 0.0075874 v FourierNb 4.5082e-05 212.09 1.8586 0.090572 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.897 533.96 403.11 421.97 v Boundary Density 0.39801 4.5427 0.98498 0.89768 v Yplus 0 43.749 2.4477 0.95311 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8159e-05 43.617 0.47665 0.010611 INSTANT 0.158909405E-01 TIME STEP NUMBER 30091 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.649380851E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560710995E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121714091E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10349E+01 0.57881E+02 Friction velocity uk : 0.10349E+01 0.57881E+02 Dimensionless distance yplus : 0.20573E-01 0.43769E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14449E-01 0.12468E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60103E+03 2 0.25098E-06 0.44295E+02 0.16082E+03 c Velocity[X] 0.26815E+01 c Velocity[Y] 0.11051E+02 c Velocity[Z] 0.30562E+02 c Pressure 0.75628E-01 5 0.98983E-08 0.19513E+07 0.36765E+02 c k 0.24439E+04 1 0.12768E-05 0.75985E+05 0.14009E+04 c omega 0.81513E+09 1 0.50338E-08 0.44991E+12 0.49117E+02 c TotEner 0.24211E+06 1 0.11409E-05 0.40953E+07 0.22034E+02 c temperature 0.00000E+00 0 0.00000E+00 0.75624E+01 0.22185E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.018e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.17 225.17 0.0016834 0.00079126 v Velocity[Y] -0.13029 701.9 250.49 80.962 v Velocity[Z] -19.22 355.03 24.759 1.9543 v ǁVelocityǁ 0.033484 701.9 259.94 83.704 v Pressure 51263 1.1025e+05 1.0361e+05 1.0417e+05 v k 1.1815e-08 41154 908.87 355.46 v omega 153.99 9.6781e+09 1.8458e+08 3.4143e+05 v TotEner 95183 6.2951e+05 3.4157e+05 2.4852e+05 v temperature 67.775 533.96 397.99 337.18 v Density 0.39771 4.5513 0.94932 1.0904 v TurbVisc 8.799e-19 0.064123 0.010065 0.028631 v CourantNb 1.2983e-05 42.904 0.38684 0.0075875 v FourierNb 4.5081e-05 211.93 1.858 0.090573 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.837 533.96 403.1 421.97 v Boundary Density 0.39786 4.547 0.98505 0.89769 v Yplus 0 43.769 2.4478 0.95317 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8165e-05 43.629 0.47676 0.010611 INSTANT 0.158912035E-01 TIME STEP NUMBER 30092 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.650134808E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560710542E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121737535E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10349E+01 0.57887E+02 Friction velocity uk : 0.10349E+01 0.57887E+02 Dimensionless distance yplus : 0.20572E-01 0.43789E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14449E-01 0.12469E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60103E+03 2 0.25082E-06 0.44058E+02 0.16039E+03 c Velocity[X] 0.26376E+01 c Velocity[Y] 0.11035E+02 c Velocity[Z] 0.30385E+02 c Pressure 0.75632E-01 8 0.97615E-08 0.19370E+07 0.36631E+02 c k 0.24442E+04 1 0.12781E-05 0.76077E+05 0.14016E+04 c omega 0.81513E+09 1 0.49621E-08 0.43742E+12 0.48431E+02 c TotEner 0.24211E+06 1 0.11401E-05 0.40943E+07 0.22031E+02 c temperature 0.00000E+00 0 0.00000E+00 0.75531E+01 0.22172E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0172e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.21 225.22 0.0016854 0.00079476 v Velocity[Y] -0.13029 701.9 250.49 80.963 v Velocity[Z] -19.22 355.17 24.765 1.9545 v ǁVelocityǁ 0.035703 701.9 259.95 83.705 v Pressure 51241 1.1025e+05 1.0361e+05 1.0417e+05 v k 1.1815e-08 41172 908.91 355.46 v omega 153.99 9.6781e+09 1.8458e+08 3.4143e+05 v TotEner 95137 6.2951e+05 3.4157e+05 2.4852e+05 v temperature 67.714 533.96 397.99 337.18 v Density 0.39757 4.5555 0.94931 1.0904 v TurbVisc 8.7985e-19 0.064123 0.010064 0.028632 v CourantNb 1.2988e-05 42.915 0.38693 0.0075877 v FourierNb 4.508e-05 211.78 1.8575 0.090574 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.775 533.96 403.1 421.97 v Boundary Density 0.39771 4.5513 0.98512 0.89771 v Yplus 0 43.789 2.4478 0.95323 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8172e-05 43.64 0.47686 0.010611 INSTANT 0.158914665E-01 TIME STEP NUMBER 30093 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.650849958E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560710433E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121765293E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10349E+01 0.57892E+02 Friction velocity uk : 0.10349E+01 0.57892E+02 Dimensionless distance yplus : 0.20572E-01 0.43810E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14448E-01 0.12470E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60104E+03 2 0.25066E-06 0.43828E+02 0.15997E+03 c Velocity[X] 0.25951E+01 c Velocity[Y] 0.11012E+02 c Velocity[Z] 0.30221E+02 c Pressure 0.75636E-01 8 0.98246E-08 0.19228E+07 0.36496E+02 c k 0.24444E+04 1 0.12778E-05 0.76119E+05 0.14019E+04 c omega 0.81513E+09 1 0.45833E-08 0.37980E+12 0.45128E+02 c TotEner 0.24212E+06 1 0.11393E-05 0.40938E+07 0.22030E+02 c temperature 0.00000E+00 0 0.00000E+00 0.75476E+01 0.22164E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0164e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.26 225.26 0.0016874 0.00079827 v Velocity[Y] -0.13028 701.9 250.49 80.964 v Velocity[Z] -19.219 355.32 24.771 1.9547 v ǁVelocityǁ 0.038007 701.9 259.95 83.706 v Pressure 51219 1.1025e+05 1.0361e+05 1.0417e+05 v k 1.1814e-08 41190 908.96 355.46 v omega 154 9.6781e+09 1.8458e+08 3.4143e+05 v TotEner 95091 6.2951e+05 3.4157e+05 2.4852e+05 v temperature 67.652 533.96 397.99 337.18 v Density 0.39742 4.5598 0.94931 1.0904 v TurbVisc 8.7982e-19 0.064123 0.010064 0.028632 v CourantNb 1.2992e-05 42.927 0.38703 0.0075878 v FourierNb 4.508e-05 211.62 1.8569 0.090574 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.714 533.96 403.09 421.97 v Boundary Density 0.39757 4.5555 0.98519 0.89772 v Yplus 0 43.81 2.4478 0.9533 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8178e-05 43.651 0.47696 0.010612 INSTANT 0.158917295E-01 TIME STEP NUMBER 30094 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.651525998E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560710689E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121797069E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10349E+01 0.57898E+02 Friction velocity uk : 0.10349E+01 0.57898E+02 Dimensionless distance yplus : 0.20571E-01 0.43830E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14448E-01 0.12471E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60104E+03 2 0.25050E-06 0.43635E+02 0.15962E+03 c Velocity[X] 0.25541E+01 c Velocity[Y] 0.11012E+02 c Velocity[Z] 0.30069E+02 c Pressure 0.75640E-01 5 0.96733E-08 0.19090E+07 0.36365E+02 c k 0.24447E+04 1 0.12780E-05 0.76186E+05 0.14024E+04 c omega 0.81513E+09 1 0.48230E-08 0.42014E+12 0.47464E+02 c TotEner 0.24212E+06 1 0.11386E-05 0.41019E+07 0.22051E+02 c temperature 0.00000E+00 0 0.00000E+00 0.75479E+01 0.22164E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0157e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.3 225.3 0.0016891 0.00080176 v Velocity[Y] -0.13028 701.9 250.49 80.965 v Velocity[Z] -19.219 355.46 24.776 1.9548 v ǁVelocityǁ 0.040387 701.9 259.96 83.707 v Pressure 51198 1.1025e+05 1.036e+05 1.0417e+05 v k 1.1814e-08 41208 909 355.46 v omega 154 9.6781e+09 1.8458e+08 3.4143e+05 v TotEner 95045 6.2951e+05 3.4157e+05 2.4852e+05 v temperature 67.59 533.96 397.99 337.18 v Density 0.39728 4.5641 0.9493 1.0904 v TurbVisc 8.7978e-19 0.064123 0.010064 0.028632 v CourantNb 1.2997e-05 42.938 0.38712 0.007588 v FourierNb 4.5079e-05 211.47 1.8564 0.090575 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.652 533.96 403.09 421.97 v Boundary Density 0.39742 4.5598 0.98525 0.89773 v Yplus 0 43.83 2.4478 0.95336 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8184e-05 43.662 0.47707 0.010612 INSTANT 0.158919925E-01 TIME STEP NUMBER 30095 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.652162685E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560711305E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121832560E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10349E+01 0.57903E+02 Friction velocity uk : 0.10349E+01 0.57903E+02 Dimensionless distance yplus : 0.20571E-01 0.43850E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14448E-01 0.12472E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60104E+03 2 0.25035E-06 0.43453E+02 0.15928E+03 c Velocity[X] 0.25144E+01 c Velocity[Y] 0.11011E+02 c Velocity[Z] 0.29928E+02 c Pressure 0.75644E-01 5 0.98802E-08 0.18958E+07 0.36239E+02 c k 0.24449E+04 1 0.12777E-05 0.76223E+05 0.14027E+04 c omega 0.81513E+09 1 0.48697E-08 0.45953E+12 0.49640E+02 c TotEner 0.24212E+06 1 0.11379E-05 0.41101E+07 0.22073E+02 c temperature 0.00000E+00 0 0.00000E+00 0.75510E+01 0.22169E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0149e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.34 225.34 0.001691 0.00080526 v Velocity[Y] -0.13027 701.9 250.49 80.966 v Velocity[Z] -19.218 355.61 24.782 1.955 v ǁVelocityǁ 0.042837 701.9 259.96 83.708 v Pressure 51177 1.1024e+05 1.036e+05 1.0417e+05 v k 1.1813e-08 41226 909.04 355.46 v omega 154.01 9.6781e+09 1.8458e+08 3.4143e+05 v TotEner 94999 6.2951e+05 3.4157e+05 2.4852e+05 v temperature 67.528 533.96 397.98 337.18 v Density 0.39714 4.5684 0.9493 1.0904 v TurbVisc 8.7973e-19 0.064123 0.010064 0.028632 v CourantNb 1.3001e-05 42.949 0.38721 0.0075881 v FourierNb 4.5078e-05 211.33 1.8558 0.090576 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.59 533.96 403.08 421.97 v Boundary Density 0.39728 4.5641 0.98532 0.89774 v Yplus 0 43.85 2.4478 0.95342 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8191e-05 43.672 0.47717 0.010612 INSTANT 0.158922555E-01 TIME STEP NUMBER 30096 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.652759827E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560712274E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121871462E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10348E+01 0.57908E+02 Friction velocity uk : 0.10348E+01 0.57908E+02 Dimensionless distance yplus : 0.20571E-01 0.43870E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14448E-01 0.12474E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60104E+03 2 0.25019E-06 0.43278E+02 0.15896E+03 c Velocity[X] 0.24761E+01 c Velocity[Y] 0.11005E+02 c Velocity[Z] 0.29797E+02 c Pressure 0.75648E-01 5 0.99392E-08 0.18831E+07 0.36117E+02 c k 0.24452E+04 1 0.12769E-05 0.76235E+05 0.14027E+04 c omega 0.81513E+09 1 0.47853E-08 0.44722E+12 0.48970E+02 c TotEner 0.24212E+06 1 0.11372E-05 0.41189E+07 0.22097E+02 c temperature 0.00000E+00 0 0.00000E+00 0.75563E+01 0.22176E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0142e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.38 225.38 0.001693 0.00080876 v Velocity[Y] -0.13027 701.9 250.49 80.967 v Velocity[Z] -19.218 355.75 24.788 1.9552 v ǁVelocityǁ 0.045349 701.9 259.96 83.709 v Pressure 51156 1.1024e+05 1.036e+05 1.0417e+05 v k 1.1812e-08 41244 909.08 355.46 v omega 154.01 9.6781e+09 1.8458e+08 3.4143e+05 v TotEner 94953 6.2951e+05 3.4157e+05 2.4852e+05 v temperature 67.465 533.96 397.98 337.18 v Density 0.397 4.5727 0.9493 1.0904 v TurbVisc 8.7968e-19 0.064123 0.010064 0.028632 v CourantNb 1.3006e-05 42.96 0.3873 0.0075883 v FourierNb 4.5078e-05 211.18 1.8553 0.090576 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.528 533.96 403.08 421.96 v Boundary Density 0.39714 4.5684 0.98539 0.89776 v Yplus 0 43.87 2.4478 0.95349 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8197e-05 43.683 0.47727 0.010612 INSTANT 0.158925184E-01 TIME STEP NUMBER 30097 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.653317284E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560713605E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121913473E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10348E+01 0.57913E+02 Friction velocity uk : 0.10348E+01 0.57913E+02 Dimensionless distance yplus : 0.20570E-01 0.43891E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14447E-01 0.12475E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60104E+03 2 0.25004E-06 0.43120E+02 0.15867E+03 c Velocity[X] 0.24390E+01 c Velocity[Y] 0.11005E+02 c Velocity[Z] 0.29676E+02 c Pressure 0.75652E-01 5 0.97144E-08 0.18711E+07 0.36002E+02 c k 0.24455E+04 1 0.12761E-05 0.76255E+05 0.14028E+04 c omega 0.81513E+09 1 0.46762E-08 0.50847E+12 0.52216E+02 c TotEner 0.24212E+06 1 0.11366E-05 0.41301E+07 0.22127E+02 c temperature 0.00000E+00 0 0.00000E+00 0.75639E+01 0.22187E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0135e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.42 225.42 0.0016951 0.00081225 v Velocity[Y] -0.13027 701.9 250.49 80.968 v Velocity[Z] -19.217 355.89 24.793 1.9554 v ǁVelocityǁ 0.047919 701.9 259.97 83.71 v Pressure 51135 1.1024e+05 1.036e+05 1.0417e+05 v k 1.1812e-08 41262 909.12 355.46 v omega 154.02 9.6781e+09 1.8458e+08 3.4143e+05 v TotEner 94906 6.2951e+05 3.4157e+05 2.4852e+05 v temperature 67.402 533.96 397.98 337.18 v Density 0.39686 4.577 0.94929 1.0904 v TurbVisc 8.7963e-19 0.064123 0.010064 0.028632 v CourantNb 1.301e-05 42.971 0.3874 0.0075884 v FourierNb 4.5077e-05 211.04 1.8548 0.090577 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.465 533.96 403.07 421.96 v Boundary Density 0.397 4.5727 0.98546 0.89777 v Yplus 0 43.891 2.4478 0.95355 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8203e-05 43.693 0.47736 0.010612 INSTANT 0.158927814E-01 TIME STEP NUMBER 30098 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.653834971E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560715304E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121958294E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10348E+01 0.57919E+02 Friction velocity uk : 0.10348E+01 0.57919E+02 Dimensionless distance yplus : 0.20570E-01 0.43911E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14447E-01 0.12476E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60105E+03 2 0.24989E-06 0.42972E+02 0.15839E+03 c Velocity[X] 0.24031E+01 c Velocity[Y] 0.11005E+02 c Velocity[Z] 0.29564E+02 c Pressure 0.75656E-01 8 0.99134E-08 0.18600E+07 0.35895E+02 c k 0.24457E+04 1 0.12750E-05 0.76245E+05 0.14026E+04 c omega 0.81513E+09 1 0.50074E-08 0.50223E+12 0.51894E+02 c TotEner 0.24212E+06 1 0.11360E-05 0.41424E+07 0.22160E+02 c temperature 0.00000E+00 0 0.00000E+00 0.75732E+01 0.22201E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0128e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.46 225.46 0.0016972 0.00081574 v Velocity[Y] -0.13026 701.9 250.49 80.969 v Velocity[Z] -19.217 356.03 24.799 1.9556 v ǁVelocityǁ 0.050542 701.9 259.97 83.71 v Pressure 51114 1.1024e+05 1.036e+05 1.0417e+05 v k 1.1811e-08 41280 909.16 355.46 v omega 154.02 9.6781e+09 1.8458e+08 3.4143e+05 v TotEner 94860 6.2951e+05 3.4157e+05 2.4852e+05 v temperature 67.338 533.96 397.98 337.18 v Density 0.39673 4.5813 0.94929 1.0904 v TurbVisc 8.7958e-19 0.064123 0.010064 0.028633 v CourantNb 1.3015e-05 42.981 0.38748 0.0075886 v FourierNb 4.5076e-05 210.9 1.8543 0.090578 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.402 533.96 403.07 421.96 v Boundary Density 0.39686 4.577 0.98552 0.89778 v Yplus 0 43.911 2.4479 0.95361 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8209e-05 43.704 0.47746 0.010613 INSTANT 0.158930444E-01 TIME STEP NUMBER 30099 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.654312855E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560717374E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122005627E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10348E+01 0.57924E+02 Friction velocity uk : 0.10348E+01 0.57924E+02 Dimensionless distance yplus : 0.20569E-01 0.43931E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14447E-01 0.12477E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60105E+03 2 0.24974E-06 0.42842E+02 0.15815E+03 c Velocity[X] 0.23684E+01 c Velocity[Y] 0.11014E+02 c Velocity[Z] 0.29460E+02 c Pressure 0.75660E-01 8 0.96362E-08 0.18497E+07 0.35796E+02 c k 0.24460E+04 1 0.12739E-05 0.76265E+05 0.14027E+04 c omega 0.81513E+09 1 0.49275E-08 0.44405E+12 0.48796E+02 c TotEner 0.24213E+06 1 0.11355E-05 0.41577E+07 0.22201E+02 c temperature 0.00000E+00 0 0.00000E+00 0.75847E+01 0.22218E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0121e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.5 225.5 0.0016992 0.00081923 v Velocity[Y] -0.13026 701.9 250.5 80.97 v Velocity[Z] -19.216 356.18 24.805 1.9557 v ǁVelocityǁ 0.053215 701.9 259.98 83.711 v Pressure 51094 1.1024e+05 1.036e+05 1.0417e+05 v k 1.1811e-08 41298 909.2 355.45 v omega 154.03 9.6781e+09 1.8458e+08 3.4143e+05 v TotEner 94813 6.2951e+05 3.4158e+05 2.4852e+05 v temperature 67.274 533.96 397.98 337.18 v Density 0.39659 4.5855 0.94928 1.0904 v TurbVisc 8.7955e-19 0.064123 0.010064 0.028633 v CourantNb 1.3019e-05 42.992 0.38757 0.0075887 v FourierNb 4.5076e-05 210.76 1.8538 0.090579 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.338 533.96 403.07 421.96 v Boundary Density 0.39673 4.5813 0.98559 0.89779 v Yplus 0 43.931 2.4479 0.95368 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8215e-05 43.714 0.47755 0.010613 INSTANT 0.158933074E-01 TIME STEP NUMBER 30100 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.654750952E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560719815E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122055185E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10348E+01 0.57929E+02 Friction velocity uk : 0.10348E+01 0.57929E+02 Dimensionless distance yplus : 0.20569E-01 0.43952E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14446E-01 0.12478E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60105E+03 2 0.24959E-06 0.42724E+02 0.15793E+03 c Velocity[X] 0.23347E+01 c Velocity[Y] 0.11026E+02 c Velocity[Z] 0.29364E+02 c Pressure 0.75664E-01 8 0.93921E-08 0.18401E+07 0.35703E+02 c k 0.24463E+04 1 0.12727E-05 0.76288E+05 0.14028E+04 c omega 0.81513E+09 1 0.49983E-08 0.43639E+12 0.48373E+02 c TotEner 0.24213E+06 1 0.11350E-05 0.41731E+07 0.22241E+02 c temperature 0.00000E+00 0 0.00000E+00 0.75963E+01 0.22235E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0114e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.53 225.54 0.0017011 0.0008227 v Velocity[Y] -0.13025 701.9 250.5 80.971 v Velocity[Z] -19.215 356.32 24.81 1.9559 v ǁVelocityǁ 0.055934 701.9 259.98 83.712 v Pressure 51074 1.1024e+05 1.036e+05 1.0417e+05 v k 1.181e-08 41316 909.24 355.45 v omega 154.03 9.6781e+09 1.8458e+08 3.4143e+05 v TotEner 94766 6.2951e+05 3.4158e+05 2.4852e+05 v temperature 67.21 533.96 397.98 337.18 v Density 0.39646 4.5898 0.94928 1.0904 v TurbVisc 8.7952e-19 0.064122 0.010064 0.028633 v CourantNb 1.3023e-05 43.002 0.38766 0.0075888 v FourierNb 4.5075e-05 210.62 1.8533 0.090579 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.274 533.96 403.06 421.96 v Boundary Density 0.39659 4.5855 0.98566 0.89781 v Yplus 0 43.952 2.4479 0.95374 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8221e-05 43.724 0.47765 0.010613 INSTANT 0.158935704E-01 TIME STEP NUMBER 30101 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.655149335E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560722611E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122106687E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10347E+01 0.57934E+02 Friction velocity uk : 0.10347E+01 0.57934E+02 Dimensionless distance yplus : 0.20568E-01 0.43972E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14446E-01 0.12479E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60105E+03 2 0.24945E-06 0.42583E+02 0.15767E+03 c Velocity[X] 0.23019E+01 c Velocity[Y] 0.11007E+02 c Velocity[Z] 0.29274E+02 c Pressure 0.75668E-01 8 0.93920E-08 0.18319E+07 0.35623E+02 c k 0.24465E+04 1 0.12696E-05 0.76214E+05 0.14020E+04 c omega 0.81513E+09 1 0.49900E-08 0.50412E+12 0.51992E+02 c TotEner 0.24213E+06 1 0.11344E-05 0.41822E+07 0.22266E+02 c temperature 0.00000E+00 0 0.00000E+00 0.76074E+01 0.22251E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0107e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.57 225.57 0.0017028 0.00082616 v Velocity[Y] -0.13025 701.9 250.5 80.972 v Velocity[Z] -19.215 356.45 24.816 1.9561 v ǁVelocityǁ 0.058698 701.9 259.99 83.713 v Pressure 51054 1.1024e+05 1.036e+05 1.0417e+05 v k 1.181e-08 41334 909.28 355.45 v omega 154.04 9.6782e+09 1.8458e+08 3.4143e+05 v TotEner 94718 6.2951e+05 3.4158e+05 2.4852e+05 v temperature 67.145 533.96 397.98 337.18 v Density 0.39633 4.5941 0.94927 1.0904 v TurbVisc 8.7948e-19 0.064122 0.010064 0.028633 v CourantNb 1.3027e-05 43.013 0.38775 0.007589 v FourierNb 4.5074e-05 210.49 1.8528 0.09058 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.21 533.96 403.06 421.96 v Boundary Density 0.39646 4.5898 0.98572 0.89782 v Yplus 0 43.972 2.4479 0.9538 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8227e-05 43.734 0.47774 0.010613 INSTANT 0.158938334E-01 TIME STEP NUMBER 30102 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.655508126E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560725770E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122159860E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10347E+01 0.57938E+02 Friction velocity uk : 0.10347E+01 0.57938E+02 Dimensionless distance yplus : 0.20568E-01 0.43992E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14446E-01 0.12480E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60105E+03 2 0.24930E-06 0.42464E+02 0.15745E+03 c Velocity[X] 0.22699E+01 c Velocity[Y] 0.11002E+02 c Velocity[Z] 0.29192E+02 c Pressure 0.75672E-01 8 0.96093E-08 0.18245E+07 0.35551E+02 c k 0.24468E+04 1 0.12672E-05 0.76201E+05 0.14018E+04 c omega 0.81513E+09 1 0.46219E-08 0.41609E+12 0.47235E+02 c TotEner 0.24213E+06 1 0.11339E-05 0.41951E+07 0.22300E+02 c temperature 0.00000E+00 0 0.00000E+00 0.76204E+01 0.22270E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.01e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.61 225.61 0.0017045 0.00082962 v Velocity[Y] -0.13025 701.9 250.5 80.973 v Velocity[Z] -19.214 356.59 24.821 1.9563 v ǁVelocityǁ 0.061503 701.9 259.99 83.714 v Pressure 51035 1.1024e+05 1.036e+05 1.0417e+05 v k 1.1809e-08 41352 909.32 355.45 v omega 154.04 9.6782e+09 1.8458e+08 3.4143e+05 v TotEner 94670 6.2951e+05 3.4158e+05 2.4852e+05 v temperature 67.079 533.96 397.98 337.18 v Density 0.3962 4.5984 0.94927 1.0904 v TurbVisc 8.7944e-19 0.064122 0.010064 0.028633 v CourantNb 1.3031e-05 43.023 0.38783 0.0075891 v FourierNb 4.5074e-05 210.36 1.8523 0.090581 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.145 533.96 403.05 421.96 v Boundary Density 0.39633 4.5941 0.98579 0.89783 v Yplus 0 43.992 2.4479 0.95386 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8233e-05 43.744 0.47783 0.010613 INSTANT 0.158940964E-01 TIME STEP NUMBER 30103 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.655827496E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560729288E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122214442E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10347E+01 0.57943E+02 Friction velocity uk : 0.10347E+01 0.57943E+02 Dimensionless distance yplus : 0.20568E-01 0.44013E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14445E-01 0.12481E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60105E+03 2 0.24916E-06 0.42353E+02 0.15724E+03 c Velocity[X] 0.22387E+01 c Velocity[Y] 0.10998E+02 c Velocity[Z] 0.29116E+02 c Pressure 0.75676E-01 8 0.97017E-08 0.18179E+07 0.35487E+02 c k 0.24470E+04 1 0.12652E-05 0.76228E+05 0.14019E+04 c omega 0.81513E+09 1 0.43689E-08 0.35276E+12 0.43492E+02 c TotEner 0.24213E+06 1 0.11333E-05 0.42076E+07 0.22333E+02 c temperature 0.00000E+00 0 0.00000E+00 0.76332E+01 0.22289E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0094e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.65 225.65 0.0017062 0.00083307 v Velocity[Y] -0.13024 701.9 250.5 80.974 v Velocity[Z] -19.214 356.73 24.827 1.9565 v ǁVelocityǁ 0.064349 701.9 259.99 83.715 v Pressure 51015 1.1024e+05 1.0359e+05 1.0417e+05 v k 1.1809e-08 41370 909.36 355.45 v omega 154.05 9.6782e+09 1.8458e+08 3.4143e+05 v TotEner 94622 6.2951e+05 3.4158e+05 2.4852e+05 v temperature 67.013 533.96 397.97 337.18 v Density 0.39607 4.6026 0.94927 1.0904 v TurbVisc 8.794e-19 0.064122 0.010064 0.028633 v CourantNb 1.3035e-05 43.033 0.38792 0.0075893 v FourierNb 4.5073e-05 210.23 1.8519 0.090582 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.079 533.96 403.05 421.96 v Boundary Density 0.3962 4.5984 0.98586 0.89784 v Yplus 0 44.013 2.4479 0.95392 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8239e-05 43.753 0.47792 0.010614 INSTANT 0.158943594E-01 TIME STEP NUMBER 30104 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656107665E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560733156E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122270184E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10347E+01 0.57948E+02 Friction velocity uk : 0.10347E+01 0.57948E+02 Dimensionless distance yplus : 0.20567E-01 0.44033E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14445E-01 0.12482E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60106E+03 2 0.24901E-06 0.42260E+02 0.15707E+03 c Velocity[X] 0.22082E+01 c Velocity[Y] 0.11006E+02 c Velocity[Z] 0.29046E+02 c Pressure 0.75680E-01 9 0.87318E-08 0.18126E+07 0.35434E+02 c k 0.24473E+04 1 0.12632E-05 0.76243E+05 0.14020E+04 c omega 0.81513E+09 1 0.44207E-08 0.34606E+12 0.43077E+02 c TotEner 0.24213E+06 1 0.11329E-05 0.42234E+07 0.22375E+02 c temperature 0.00000E+00 0 0.00000E+00 0.76479E+01 0.22310E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0087e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.68 225.69 0.0017079 0.00083653 v Velocity[Y] -0.13024 701.9 250.5 80.975 v Velocity[Z] -19.213 356.87 24.832 1.9567 v ǁVelocityǁ 0.067233 701.9 260 83.716 v Pressure 50996 1.1024e+05 1.0359e+05 1.0417e+05 v k 1.1808e-08 41387 909.4 355.45 v omega 154.05 9.6782e+09 1.8458e+08 3.4143e+05 v TotEner 94574 6.2951e+05 3.4158e+05 2.4852e+05 v temperature 66.946 533.96 397.97 337.18 v Density 0.39594 4.6069 0.94926 1.0904 v TurbVisc 8.7936e-19 0.064122 0.010064 0.028633 v CourantNb 1.3039e-05 43.043 0.388 0.0075894 v FourierNb 4.5073e-05 210.1 1.8514 0.090583 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 67.013 533.96 403.04 421.96 v Boundary Density 0.39607 4.6026 0.98592 0.89786 v Yplus 0 44.033 2.4479 0.95398 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8244e-05 43.763 0.47801 0.010614 INSTANT 0.158946224E-01 TIME STEP NUMBER 30105 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656348904E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560737369E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122326848E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10347E+01 0.57953E+02 Friction velocity uk : 0.10347E+01 0.57953E+02 Dimensionless distance yplus : 0.20567E-01 0.44053E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14445E-01 0.12483E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60106E+03 2 0.24887E-06 0.42157E+02 0.15688E+03 c Velocity[X] 0.21783E+01 c Velocity[Y] 0.10997E+02 c Velocity[Z] 0.28981E+02 c Pressure 0.75684E-01 9 0.90321E-08 0.18083E+07 0.35393E+02 c k 0.24476E+04 1 0.12605E-05 0.76226E+05 0.14017E+04 c omega 0.81513E+09 1 0.43577E-08 0.39731E+12 0.46156E+02 c TotEner 0.24213E+06 1 0.11324E-05 0.42352E+07 0.22406E+02 c temperature 0.00000E+00 0 0.00000E+00 0.76623E+01 0.22331E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0081e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.72 225.72 0.0017097 0.00083997 v Velocity[Y] -0.13023 701.9 250.5 80.975 v Velocity[Z] -19.213 357.01 24.837 1.9568 v ǁVelocityǁ 0.070154 701.9 260 83.717 v Pressure 50977 1.1024e+05 1.0359e+05 1.0417e+05 v k 1.1808e-08 41405 909.44 355.45 v omega 154.06 9.6782e+09 1.8458e+08 3.4143e+05 v TotEner 94525 6.2951e+05 3.4158e+05 2.4852e+05 v temperature 66.879 533.96 397.97 337.18 v Density 0.39582 4.6112 0.94926 1.0903 v TurbVisc 8.7932e-19 0.064122 0.010064 0.028634 v CourantNb 1.3043e-05 43.053 0.38809 0.0075896 v FourierNb 4.5073e-05 209.98 1.851 0.090584 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 66.946 533.96 403.04 421.96 v Boundary Density 0.39594 4.6069 0.98599 0.89787 v Yplus 0 44.053 2.448 0.95404 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.825e-05 43.772 0.4781 0.010614 INSTANT 0.158948853E-01 TIME STEP NUMBER 30106 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656551530E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560741924E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122384209E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10347E+01 0.57957E+02 Friction velocity uk : 0.10347E+01 0.57957E+02 Dimensionless distance yplus : 0.20567E-01 0.44073E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14445E-01 0.12485E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60106E+03 2 0.24873E-06 0.42066E+02 0.15670E+03 c Velocity[X] 0.21491E+01 c Velocity[Y] 0.10994E+02 c Velocity[Z] 0.28922E+02 c Pressure 0.75688E-01 9 0.87941E-08 0.18050E+07 0.35361E+02 c k 0.24478E+04 1 0.12582E-05 0.76238E+05 0.14017E+04 c omega 0.81514E+09 1 0.51911E-08 0.52814E+12 0.53216E+02 c TotEner 0.24214E+06 1 0.11319E-05 0.42491E+07 0.22443E+02 c temperature 0.00000E+00 0 0.00000E+00 0.76781E+01 0.22354E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0074e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.75 225.76 0.0017114 0.00084341 v Velocity[Y] -0.13023 701.9 250.5 80.976 v Velocity[Z] -19.212 357.14 24.843 1.957 v ǁVelocityǁ 0.07311 701.9 260.01 83.718 v Pressure 50958 1.1024e+05 1.0359e+05 1.0417e+05 v k 1.1807e-08 41422 909.48 355.45 v omega 154.06 9.6782e+09 1.8458e+08 3.4143e+05 v TotEner 94476 6.2951e+05 3.4158e+05 2.4852e+05 v temperature 66.812 533.96 397.97 337.18 v Density 0.39569 4.6154 0.94925 1.0903 v TurbVisc 8.7929e-19 0.064122 0.010064 0.028634 v CourantNb 1.3047e-05 43.063 0.38817 0.0075897 v FourierNb 4.5072e-05 209.86 1.8505 0.090585 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 66.879 533.96 403.04 421.96 v Boundary Density 0.39582 4.6112 0.98605 0.89788 v Yplus 0 44.073 2.448 0.95411 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8255e-05 43.782 0.47819 0.010614 INSTANT 0.158951483E-01 TIME STEP NUMBER 30107 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656715908E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560746822E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122442054E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10346E+01 0.57962E+02 Friction velocity uk : 0.10346E+01 0.57962E+02 Dimensionless distance yplus : 0.20566E-01 0.44094E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14445E-01 0.12486E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60106E+03 2 0.24859E-06 0.41975E+02 0.15653E+03 c Velocity[X] 0.21205E+01 c Velocity[Y] 0.10986E+02 c Velocity[Z] 0.28869E+02 c Pressure 0.75692E-01 8 0.98420E-08 0.18026E+07 0.35337E+02 c k 0.24481E+04 1 0.12557E-05 0.76252E+05 0.14018E+04 c omega 0.81514E+09 1 0.53205E-08 0.55838E+12 0.54718E+02 c TotEner 0.24214E+06 1 0.11314E-05 0.42618E+07 0.22476E+02 c temperature 0.00000E+00 0 0.00000E+00 0.76940E+01 0.22377E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0068e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.79 225.79 0.0017131 0.00084685 v Velocity[Y] -0.13023 701.9 250.5 80.977 v Velocity[Z] -19.212 357.28 24.848 1.9572 v ǁVelocityǁ 0.0761 701.9 260.01 83.719 v Pressure 50940 1.1024e+05 1.0359e+05 1.0416e+05 v k 1.1807e-08 41440 909.51 355.45 v omega 154.07 9.6782e+09 1.8458e+08 3.4143e+05 v TotEner 94427 6.2951e+05 3.4158e+05 2.4852e+05 v temperature 66.743 533.96 397.97 337.18 v Density 0.39557 4.6197 0.94925 1.0903 v TurbVisc 8.7925e-19 0.064122 0.010064 0.028634 v CourantNb 1.3051e-05 43.072 0.38825 0.0075898 v FourierNb 4.5072e-05 209.74 1.8501 0.090586 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 66.812 533.96 403.03 421.95 v Boundary Density 0.39569 4.6154 0.98612 0.89789 v Yplus 0 44.094 2.448 0.95417 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.826e-05 43.791 0.47828 0.010614 INSTANT 0.158954113E-01 TIME STEP NUMBER 30108 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656842450E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560752044E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122500185E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10346E+01 0.57967E+02 Friction velocity uk : 0.10346E+01 0.57967E+02 Dimensionless distance yplus : 0.20566E-01 0.44114E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14444E-01 0.12487E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60106E+03 2 0.24845E-06 0.41900E+02 0.15639E+03 c Velocity[X] 0.20924E+01 c Velocity[Y] 0.10987E+02 c Velocity[Z] 0.28820E+02 c Pressure 0.75696E-01 8 0.98149E-08 0.18013E+07 0.35324E+02 c k 0.24484E+04 1 0.12540E-05 0.76330E+05 0.14024E+04 c omega 0.81514E+09 1 0.56292E-08 0.54361E+12 0.53989E+02 c TotEner 0.24214E+06 1 0.11310E-05 0.42773E+07 0.22517E+02 c temperature 0.00000E+00 0 0.00000E+00 0.77118E+01 0.22403E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0061e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.82 225.83 0.0017148 0.00085027 v Velocity[Y] -0.13022 701.9 250.5 80.978 v Velocity[Z] -19.211 357.41 24.853 1.9574 v ǁVelocityǁ 0.079124 701.9 260.01 83.72 v Pressure 50921 1.1024e+05 1.0359e+05 1.0416e+05 v k 1.1806e-08 41457 909.55 355.45 v omega 154.07 9.6782e+09 1.8459e+08 3.4143e+05 v TotEner 94377 6.2951e+05 3.4158e+05 2.4852e+05 v temperature 66.675 533.96 397.97 337.18 v Density 0.39545 4.6239 0.94925 1.0903 v TurbVisc 8.7921e-19 0.064122 0.010064 0.028634 v CourantNb 1.3054e-05 43.082 0.38833 0.00759 v FourierNb 4.5071e-05 209.63 1.8497 0.090587 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 66.743 533.96 403.03 421.95 v Boundary Density 0.39557 4.6197 0.98618 0.89791 v Yplus 0 44.114 2.448 0.95423 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8266e-05 43.8 0.47836 0.010615 INSTANT 0.158956743E-01 TIME STEP NUMBER 30109 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656931615E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560757581E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122558417E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10346E+01 0.57971E+02 Friction velocity uk : 0.10346E+01 0.57971E+02 Dimensionless distance yplus : 0.20566E-01 0.44134E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14444E-01 0.12488E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60106E+03 2 0.24832E-06 0.41835E+02 0.15627E+03 c Velocity[X] 0.20651E+01 c Velocity[Y] 0.10993E+02 c Velocity[Z] 0.28777E+02 c Pressure 0.75700E-01 8 0.95255E-08 0.18009E+07 0.35321E+02 c k 0.24486E+04 1 0.12527E-05 0.76432E+05 0.14032E+04 c omega 0.81514E+09 1 0.53128E-08 0.47068E+12 0.50238E+02 c TotEner 0.24214E+06 1 0.11305E-05 0.42945E+07 0.22562E+02 c temperature 0.00000E+00 0 0.00000E+00 0.77312E+01 0.22431E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0055e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.86 225.86 0.0017166 0.00085369 v Velocity[Y] -0.13022 701.9 250.5 80.979 v Velocity[Z] -19.211 357.55 24.859 1.9576 v ǁVelocityǁ 0.08218 701.9 260.02 83.721 v Pressure 50903 1.1024e+05 1.0359e+05 1.0416e+05 v k 1.1806e-08 41475 909.59 355.45 v omega 154.08 9.6782e+09 1.8459e+08 3.4143e+05 v TotEner 94327 6.2951e+05 3.4158e+05 2.4852e+05 v temperature 66.605 533.96 397.97 337.18 v Density 0.39533 4.6282 0.94924 1.0903 v TurbVisc 8.7917e-19 0.064121 0.010064 0.028634 v CourantNb 1.3058e-05 43.092 0.38841 0.0075901 v FourierNb 4.5071e-05 209.51 1.8493 0.090588 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 66.675 533.96 403.02 421.95 v Boundary Density 0.39545 4.6239 0.98624 0.89792 v Yplus 0 44.134 2.448 0.95429 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8271e-05 43.81 0.47845 0.010615 INSTANT 0.158959373E-01 TIME STEP NUMBER 30110 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656983903E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560763419E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122616580E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10346E+01 0.57975E+02 Friction velocity uk : 0.10346E+01 0.57975E+02 Dimensionless distance yplus : 0.20565E-01 0.44154E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14444E-01 0.12489E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60107E+03 2 0.24818E-06 0.41807E+02 0.15622E+03 c Velocity[X] 0.20383E+01 c Velocity[Y] 0.11031E+02 c Velocity[Z] 0.28738E+02 c Pressure 0.75704E-01 8 0.96262E-08 0.18012E+07 0.35324E+02 c k 0.24489E+04 1 0.12522E-05 0.76580E+05 0.14045E+04 c omega 0.81514E+09 1 0.55098E-08 0.51732E+12 0.52668E+02 c TotEner 0.24214E+06 1 0.11302E-05 0.43193E+07 0.22627E+02 c temperature 0.00000E+00 0 0.00000E+00 0.77532E+01 0.22463E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0049e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.89 225.89 0.0017183 0.00085711 v Velocity[Y] -0.13022 701.9 250.5 80.98 v Velocity[Z] -19.21 357.68 24.864 1.9577 v ǁVelocityǁ 0.085268 701.9 260.02 83.722 v Pressure 50885 1.1024e+05 1.0359e+05 1.0416e+05 v k 1.1805e-08 41492 909.62 355.44 v omega 154.08 9.6782e+09 1.8459e+08 3.4143e+05 v TotEner 94277 6.2951e+05 3.4158e+05 2.4852e+05 v temperature 66.536 533.96 397.97 337.18 v Density 0.39521 4.6325 0.94924 1.0903 v TurbVisc 8.7913e-19 0.064121 0.010064 0.028634 v CourantNb 1.3062e-05 43.101 0.38849 0.0075903 v FourierNb 4.5071e-05 209.4 1.8489 0.090589 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 66.605 533.96 403.02 421.95 v Boundary Density 0.39533 4.6282 0.98631 0.89793 v Yplus 0 44.154 2.448 0.95435 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8276e-05 43.819 0.47853 0.010615 INSTANT 0.158962003E-01 TIME STEP NUMBER 30111 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656999860E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560769563E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122674516E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10346E+01 0.57980E+02 Friction velocity uk : 0.10346E+01 0.57980E+02 Dimensionless distance yplus : 0.20565E-01 0.44174E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14444E-01 0.12490E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60107E+03 2 0.24805E-06 0.41730E+02 0.15607E+03 c Velocity[X] 0.20123E+01 c Velocity[Y] 0.11014E+02 c Velocity[Z] 0.28704E+02 c Pressure 0.75708E-01 8 0.99789E-08 0.18026E+07 0.35338E+02 c k 0.24492E+04 1 0.12505E-05 0.76579E+05 0.14044E+04 c omega 0.81514E+09 1 0.49867E-08 0.42908E+12 0.47966E+02 c TotEner 0.24214E+06 1 0.11297E-05 0.43295E+07 0.22654E+02 c temperature 0.00000E+00 0 0.00000E+00 0.77714E+01 0.22489E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0043e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.93 225.93 0.0017201 0.00086052 v Velocity[Y] -0.13021 701.9 250.5 80.981 v Velocity[Z] -19.21 357.81 24.869 1.9579 v ǁVelocityǁ 0.088386 701.9 260.03 83.722 v Pressure 50866 1.1024e+05 1.0359e+05 1.0416e+05 v k 1.1805e-08 41509 909.66 355.44 v omega 154.09 9.6782e+09 1.8459e+08 3.4143e+05 v TotEner 94226 6.2951e+05 3.4158e+05 2.4852e+05 v temperature 66.465 533.96 397.96 337.18 v Density 0.39509 4.6367 0.94924 1.0903 v TurbVisc 8.791e-19 0.064121 0.010065 0.028635 v CourantNb 1.3065e-05 43.11 0.38857 0.0075904 v FourierNb 4.507e-05 209.29 1.8485 0.09059 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 66.536 533.96 403.01 421.95 v Boundary Density 0.39521 4.6325 0.98637 0.89794 v Yplus 0 44.174 2.4481 0.95441 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8281e-05 43.828 0.47862 0.010615 INSTANT 0.158964633E-01 TIME STEP NUMBER 30112 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656980073E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560775998E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122732082E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10346E+01 0.57984E+02 Friction velocity uk : 0.10346E+01 0.57984E+02 Dimensionless distance yplus : 0.20565E-01 0.44195E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14443E-01 0.12491E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60107E+03 2 0.24791E-06 0.41669E+02 0.15596E+03 c Velocity[X] 0.19868E+01 c Velocity[Y] 0.11008E+02 c Velocity[Z] 0.28674E+02 c Pressure 0.75712E-01 8 0.93157E-08 0.18044E+07 0.35355E+02 c k 0.24494E+04 1 0.12495E-05 0.76631E+05 0.14047E+04 c omega 0.81514E+09 1 0.47859E-08 0.38369E+12 0.45358E+02 c TotEner 0.24214E+06 1 0.11293E-05 0.43426E+07 0.22688E+02 c temperature 0.00000E+00 0 0.00000E+00 0.77912E+01 0.22518E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0037e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.96 225.96 0.0017221 0.00086394 v Velocity[Y] -0.13021 701.9 250.5 80.982 v Velocity[Z] -19.209 357.95 24.874 1.9581 v ǁVelocityǁ 0.091535 701.9 260.03 83.723 v Pressure 50849 1.1024e+05 1.0359e+05 1.0416e+05 v k 1.1804e-08 41527 909.69 355.44 v omega 154.09 9.6782e+09 1.8459e+08 3.4144e+05 v TotEner 94175 6.2951e+05 3.4158e+05 2.4852e+05 v temperature 66.394 533.96 397.96 337.18 v Density 0.39497 4.641 0.94923 1.0903 v TurbVisc 8.7906e-19 0.064121 0.010065 0.028635 v CourantNb 1.3068e-05 43.12 0.38865 0.0075906 v FourierNb 4.507e-05 209.18 1.8481 0.090591 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 66.465 533.96 403.01 421.95 v Boundary Density 0.39509 4.6367 0.98643 0.89796 v Yplus 0 44.195 2.4481 0.95447 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8285e-05 43.836 0.4787 0.010615 INSTANT 0.158967263E-01 TIME STEP NUMBER 30113 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656925173E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560782708E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122789148E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10346E+01 0.57989E+02 Friction velocity uk : 0.10346E+01 0.57989E+02 Dimensionless distance yplus : 0.20565E-01 0.44215E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14443E-01 0.12492E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60107E+03 2 0.24778E-06 0.41614E+02 0.15585E+03 c Velocity[X] 0.19620E+01 c Velocity[Y] 0.11003E+02 c Velocity[Z] 0.28649E+02 c Pressure 0.75716E-01 8 0.85924E-08 0.18071E+07 0.35381E+02 c k 0.24497E+04 1 0.12485E-05 0.76704E+05 0.14053E+04 c omega 0.81514E+09 1 0.59287E-08 0.47610E+12 0.50526E+02 c TotEner 0.24215E+06 1 0.11288E-05 0.43561E+07 0.22723E+02 c temperature 0.00000E+00 0 0.00000E+00 0.78120E+01 0.22548E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0031e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -225.99 225.99 0.0017243 0.00086735 v Velocity[Y] -0.1302 701.9 250.5 80.983 v Velocity[Z] -19.209 358.08 24.879 1.9583 v ǁVelocityǁ 0.094712 701.9 260.03 83.724 v Pressure 50831 1.1024e+05 1.0358e+05 1.0416e+05 v k 1.1804e-08 41544 909.73 355.44 v omega 154.1 9.6782e+09 1.8459e+08 3.4144e+05 v TotEner 94123 6.2951e+05 3.4158e+05 2.4853e+05 v temperature 66.323 533.96 397.96 337.18 v Density 0.39485 4.6452 0.94923 1.0903 v TurbVisc 8.7902e-19 0.064121 0.010065 0.028635 v CourantNb 1.3072e-05 43.129 0.38872 0.0075907 v FourierNb 4.507e-05 209.08 1.8477 0.090592 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 66.394 533.96 403 421.95 v Boundary Density 0.39497 4.641 0.98649 0.89797 v Yplus 0 44.215 2.4481 0.95453 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.829e-05 43.845 0.47878 0.010615 INSTANT 0.158969893E-01 TIME STEP NUMBER 30114 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656835830E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560789668E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122845597E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10345E+01 0.57993E+02 Friction velocity uk : 0.10345E+01 0.57993E+02 Dimensionless distance yplus : 0.20564E-01 0.44235E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14443E-01 0.12493E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60107E+03 2 0.24765E-06 0.41558E+02 0.15574E+03 c Velocity[X] 0.19378E+01 c Velocity[Y] 0.10992E+02 c Velocity[Z] 0.28628E+02 c Pressure 0.75720E-01 8 0.86177E-08 0.18104E+07 0.35414E+02 c k 0.24500E+04 1 0.12476E-05 0.76783E+05 0.14059E+04 c omega 0.81514E+09 1 0.54466E-08 0.42240E+12 0.47591E+02 c TotEner 0.24215E+06 1 0.11283E-05 0.43682E+07 0.22755E+02 c temperature 0.00000E+00 0 0.00000E+00 0.78330E+01 0.22578E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0025e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.03 226.03 0.0017263 0.00087075 v Velocity[Y] -0.1302 701.9 250.5 80.984 v Velocity[Z] -19.208 358.21 24.884 1.9585 v ǁVelocityǁ 0.097918 701.9 260.04 83.725 v Pressure 50813 1.1024e+05 1.0358e+05 1.0416e+05 v k 1.1803e-08 41561 909.76 355.44 v omega 154.1 9.6783e+09 1.8459e+08 3.4144e+05 v TotEner 94072 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 66.251 533.96 397.96 337.19 v Density 0.39473 4.6495 0.94922 1.0903 v TurbVisc 8.7898e-19 0.064121 0.010065 0.028635 v CourantNb 1.3075e-05 43.138 0.3888 0.0075908 v FourierNb 4.507e-05 208.97 1.8473 0.090594 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 66.323 533.96 403 421.95 v Boundary Density 0.39485 4.6452 0.98656 0.89798 v Yplus 0 44.235 2.4481 0.95459 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8295e-05 43.854 0.47886 0.010616 INSTANT 0.158972523E-01 TIME STEP NUMBER 30115 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656712753E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560796846E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122901324E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10345E+01 0.57997E+02 Friction velocity uk : 0.10345E+01 0.57997E+02 Dimensionless distance yplus : 0.20564E-01 0.44255E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14443E-01 0.12494E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60107E+03 2 0.24752E-06 0.41533E+02 0.15570E+03 c Velocity[X] 0.19144E+01 c Velocity[Y] 0.11007E+02 c Velocity[Z] 0.28612E+02 c Pressure 0.75724E-01 8 0.93007E-08 0.18142E+07 0.35451E+02 c k 0.24502E+04 1 0.12487E-05 0.76938E+05 0.14072E+04 c omega 0.81514E+09 1 0.53948E-08 0.42302E+12 0.47626E+02 c TotEner 0.24215E+06 1 0.11279E-05 0.43871E+07 0.22804E+02 c temperature 0.00000E+00 0 0.00000E+00 0.78563E+01 0.22612E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0019e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.06 226.06 0.0017283 0.00087414 v Velocity[Y] -0.1302 701.9 250.51 80.985 v Velocity[Z] -19.207 358.34 24.89 1.9587 v ǁVelocityǁ 0.10115 701.9 260.04 83.726 v Pressure 50795 1.1024e+05 1.0358e+05 1.0416e+05 v k 1.1803e-08 41578 909.79 355.44 v omega 154.11 9.6783e+09 1.8459e+08 3.4144e+05 v TotEner 94019 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 66.178 533.96 397.96 337.19 v Density 0.39462 4.6537 0.94922 1.0903 v TurbVisc 8.7895e-19 0.064121 0.010065 0.028635 v CourantNb 1.3078e-05 43.147 0.38888 0.007591 v FourierNb 4.507e-05 208.87 1.847 0.090595 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 66.251 533.96 402.99 421.95 v Boundary Density 0.39473 4.6495 0.98662 0.89799 v Yplus 0 44.255 2.4481 0.95465 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8299e-05 43.862 0.47894 0.010616 INSTANT 0.158975153E-01 TIME STEP NUMBER 30116 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656556692E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560804217E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122956236E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10345E+01 0.58001E+02 Friction velocity uk : 0.10345E+01 0.58001E+02 Dimensionless distance yplus : 0.20564E-01 0.44276E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14443E-01 0.12495E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60108E+03 2 0.24739E-06 0.41509E+02 0.15565E+03 c Velocity[X] 0.18916E+01 c Velocity[Y] 0.11017E+02 c Velocity[Z] 0.28601E+02 c Pressure 0.75728E-01 8 0.87317E-08 0.18190E+07 0.35498E+02 c k 0.24505E+04 1 0.12506E-05 0.77089E+05 0.14085E+04 c omega 0.81514E+09 1 0.48911E-08 0.39586E+12 0.46072E+02 c TotEner 0.24215E+06 1 0.11276E-05 0.44052E+07 0.22851E+02 c temperature 0.00000E+00 0 0.00000E+00 0.78806E+01 0.22647E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0013e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.09 226.09 0.0017302 0.00087752 v Velocity[Y] -0.13019 701.9 250.51 80.986 v Velocity[Z] -19.207 358.47 24.895 1.9588 v ǁVelocityǁ 0.10441 701.9 260.05 83.727 v Pressure 50778 1.1024e+05 1.0358e+05 1.0416e+05 v k 1.1802e-08 41595 909.83 355.44 v omega 154.11 9.6783e+09 1.8459e+08 3.4144e+05 v TotEner 93967 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 66.105 533.96 397.96 337.19 v Density 0.3945 4.658 0.94922 1.0903 v TurbVisc 8.7891e-19 0.064121 0.010065 0.028635 v CourantNb 1.3081e-05 43.156 0.38895 0.0075911 v FourierNb 4.507e-05 208.77 1.8466 0.090596 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 66.178 533.96 402.99 421.95 v Boundary Density 0.39462 4.6537 0.98668 0.898 v Yplus 0 44.276 2.4482 0.95472 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8304e-05 43.871 0.47902 0.010616 INSTANT 0.158977783E-01 TIME STEP NUMBER 30117 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656368433E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560811773E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123010253E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10345E+01 0.58006E+02 Friction velocity uk : 0.10345E+01 0.58006E+02 Dimensionless distance yplus : 0.20563E-01 0.44296E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14442E-01 0.12497E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60108E+03 2 0.24726E-06 0.41443E+02 0.15552E+03 c Velocity[X] 0.18694E+01 c Velocity[Y] 0.10980E+02 c Velocity[Z] 0.28593E+02 c Pressure 0.75732E-01 8 0.84098E-08 0.18239E+07 0.35545E+02 c k 0.24508E+04 1 0.12488E-05 0.77098E+05 0.14085E+04 c omega 0.81514E+09 1 0.45763E-08 0.43967E+12 0.48554E+02 c TotEner 0.24215E+06 1 0.11270E-05 0.44086E+07 0.22860E+02 c temperature 0.00000E+00 0 0.00000E+00 0.79000E+01 0.22675E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0007e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.12 226.12 0.0017321 0.0008809 v Velocity[Y] -0.13019 701.9 250.51 80.987 v Velocity[Z] -19.206 358.6 24.9 1.959 v ǁVelocityǁ 0.1077 701.9 260.05 83.728 v Pressure 50760 1.1024e+05 1.0358e+05 1.0416e+05 v k 1.1802e-08 41612 909.86 355.44 v omega 154.12 9.6783e+09 1.8459e+08 3.4144e+05 v TotEner 93914 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 66.032 533.96 397.96 337.19 v Density 0.39439 4.6623 0.94921 1.0903 v TurbVisc 8.7888e-19 0.06412 0.010065 0.028636 v CourantNb 1.3084e-05 43.166 0.38903 0.0075913 v FourierNb 4.5069e-05 208.67 1.8463 0.090597 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 66.105 533.96 402.98 421.95 v Boundary Density 0.3945 4.658 0.98674 0.89802 v Yplus 0 44.296 2.4482 0.95478 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8308e-05 43.879 0.4791 0.010616 INSTANT 0.158980413E-01 TIME STEP NUMBER 30118 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656148799E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560819498E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123063303E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10345E+01 0.58010E+02 Friction velocity uk : 0.10345E+01 0.58010E+02 Dimensionless distance yplus : 0.20563E-01 0.44316E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14442E-01 0.12498E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60108E+03 2 0.24713E-06 0.41416E+02 0.15547E+03 c Velocity[X] 0.18477E+01 c Velocity[Y] 0.10979E+02 c Velocity[Z] 0.28590E+02 c Pressure 0.75736E-01 8 0.87188E-08 0.18291E+07 0.35596E+02 c k 0.24510E+04 1 0.12492E-05 0.77195E+05 0.14093E+04 c omega 0.81514E+09 1 0.45501E-08 0.41527E+12 0.47188E+02 c TotEner 0.24215E+06 1 0.11265E-05 0.44220E+07 0.22895E+02 c temperature 0.00000E+00 0 0.00000E+00 0.79231E+01 0.22708E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 3.0002e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.15 226.15 0.0017339 0.00088426 v Velocity[Y] -0.13019 701.9 250.51 80.988 v Velocity[Z] -19.206 358.73 24.905 1.9592 v ǁVelocityǁ 0.11102 701.9 260.05 83.729 v Pressure 50743 1.1024e+05 1.0358e+05 1.0416e+05 v k 1.1802e-08 41629 909.89 355.44 v omega 154.12 9.6783e+09 1.8459e+08 3.4144e+05 v TotEner 93860 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 65.958 533.96 397.96 337.19 v Density 0.39427 4.6666 0.94921 1.0903 v TurbVisc 8.7884e-19 0.06412 0.010065 0.028636 v CourantNb 1.3087e-05 43.174 0.3891 0.0075914 v FourierNb 4.5069e-05 208.58 1.8459 0.090598 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 66.032 533.96 402.98 421.94 v Boundary Density 0.39439 4.6623 0.9868 0.89803 v Yplus 0 44.316 2.4482 0.95484 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8312e-05 43.888 0.47918 0.010616 INSTANT 0.158983043E-01 TIME STEP NUMBER 30119 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.655898646E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560827358E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123115328E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10345E+01 0.58014E+02 Friction velocity uk : 0.10345E+01 0.58014E+02 Dimensionless distance yplus : 0.20563E-01 0.44336E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14442E-01 0.12499E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60108E+03 2 0.24700E-06 0.41393E+02 0.15543E+03 c Velocity[X] 0.18266E+01 c Velocity[Y] 0.10975E+02 c Velocity[Z] 0.28591E+02 c Pressure 0.75740E-01 8 0.87529E-08 0.18351E+07 0.35654E+02 c k 0.24513E+04 1 0.12505E-05 0.77317E+05 0.14103E+04 c omega 0.81514E+09 1 0.43248E-08 0.36559E+12 0.44275E+02 c TotEner 0.24215E+06 1 0.11261E-05 0.44350E+07 0.22928E+02 c temperature 0.00000E+00 0 0.00000E+00 0.79468E+01 0.22741E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9996e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.18 226.19 0.0017358 0.00088762 v Velocity[Y] -0.13018 701.9 250.51 80.989 v Velocity[Z] -19.205 358.86 24.91 1.9594 v ǁVelocityǁ 0.11436 701.9 260.06 83.73 v Pressure 50726 1.1024e+05 1.0358e+05 1.0416e+05 v k 1.1801e-08 41646 909.93 355.44 v omega 154.13 9.6783e+09 1.8459e+08 3.4143e+05 v TotEner 93807 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 65.883 533.96 397.95 337.19 v Density 0.39416 4.6709 0.9492 1.0903 v TurbVisc 8.7881e-19 0.06412 0.010065 0.028636 v CourantNb 1.309e-05 43.183 0.38918 0.0075915 v FourierNb 4.5069e-05 208.48 1.8456 0.090599 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 65.958 533.96 402.98 421.94 v Boundary Density 0.39427 4.6666 0.98686 0.89804 v Yplus 0 44.336 2.4482 0.9549 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8316e-05 43.896 0.47926 0.010617 INSTANT 0.158985673E-01 TIME STEP NUMBER 30120 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.655618866E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560835319E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123166277E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10345E+01 0.58018E+02 Friction velocity uk : 0.10345E+01 0.58018E+02 Dimensionless distance yplus : 0.20562E-01 0.44357E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14442E-01 0.12500E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60108E+03 2 0.24688E-06 0.41366E+02 0.15538E+03 c Velocity[X] 0.18060E+01 c Velocity[Y] 0.10964E+02 c Velocity[Z] 0.28597E+02 c Pressure 0.75744E-01 8 0.87097E-08 0.18413E+07 0.35715E+02 c k 0.24516E+04 1 0.12521E-05 0.77432E+05 0.14112E+04 c omega 0.81514E+09 1 0.48919E-08 0.54332E+12 0.53975E+02 c TotEner 0.24216E+06 1 0.11256E-05 0.44453E+07 0.22955E+02 c temperature 0.00000E+00 0 0.00000E+00 0.79698E+01 0.22774E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.999e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.22 226.22 0.0017377 0.00089096 v Velocity[Y] -0.13018 701.9 250.51 80.99 v Velocity[Z] -19.205 358.99 24.915 1.9596 v ǁVelocityǁ 0.11772 701.9 260.06 83.731 v Pressure 50709 1.1024e+05 1.0358e+05 1.0416e+05 v k 1.1801e-08 41663 909.96 355.43 v omega 154.13 9.6783e+09 1.8459e+08 3.4143e+05 v TotEner 93753 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 65.809 533.95 397.95 337.19 v Density 0.39405 4.6752 0.9492 1.0903 v TurbVisc 8.7877e-19 0.06412 0.010065 0.028636 v CourantNb 1.3093e-05 43.192 0.38925 0.0075917 v FourierNb 4.5069e-05 208.39 1.8452 0.090601 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 65.883 533.96 402.97 421.94 v Boundary Density 0.39416 4.6709 0.98692 0.89805 v Yplus 0 44.357 2.4483 0.95496 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.832e-05 43.904 0.47934 0.010617 INSTANT 0.158988303E-01 TIME STEP NUMBER 30121 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.655310383E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560843345E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123216109E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10344E+01 0.58022E+02 Friction velocity uk : 0.10344E+01 0.58022E+02 Dimensionless distance yplus : 0.20562E-01 0.44377E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14442E-01 0.12501E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60108E+03 2 0.24675E-06 0.41355E+02 0.15535E+03 c Velocity[X] 0.17860E+01 c Velocity[Y] 0.10962E+02 c Velocity[Z] 0.28607E+02 c Pressure 0.75748E-01 5 0.97381E-08 0.18482E+07 0.35781E+02 c k 0.24518E+04 1 0.12541E-05 0.77568E+05 0.14124E+04 c omega 0.81514E+09 1 0.45077E-08 0.41042E+12 0.46911E+02 c TotEner 0.24216E+06 1 0.11252E-05 0.44588E+07 0.22990E+02 c temperature 0.00000E+00 0 0.00000E+00 0.79950E+01 0.22810E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9985e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.25 226.25 0.0017396 0.0008943 v Velocity[Y] -0.13017 701.9 250.51 80.991 v Velocity[Z] -19.204 359.12 24.92 1.9598 v ǁVelocityǁ 0.12111 701.9 260.07 83.732 v Pressure 50692 1.1024e+05 1.0358e+05 1.0416e+05 v k 1.18e-08 41680 910 355.43 v omega 154.14 9.6783e+09 1.8459e+08 3.4143e+05 v TotEner 93698 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 65.733 533.95 397.95 337.19 v Density 0.39393 4.6795 0.9492 1.0903 v TurbVisc 8.7874e-19 0.06412 0.010065 0.028636 v CourantNb 1.3096e-05 43.201 0.38933 0.0075918 v FourierNb 4.5069e-05 208.3 1.8449 0.090602 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 65.809 533.95 402.97 421.94 v Boundary Density 0.39405 4.6752 0.98698 0.89807 v Yplus 0 44.377 2.4483 0.95502 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8324e-05 43.912 0.47941 0.010617 INSTANT 0.158990933E-01 TIME STEP NUMBER 30122 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.654974153E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560851413E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123264791E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10344E+01 0.58026E+02 Friction velocity uk : 0.10344E+01 0.58026E+02 Dimensionless distance yplus : 0.20562E-01 0.44398E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14441E-01 0.12502E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60109E+03 2 0.24662E-06 0.41350E+02 0.15534E+03 c Velocity[X] 0.17664E+01 c Velocity[Y] 0.10962E+02 c Velocity[Z] 0.28622E+02 c Pressure 0.75752E-01 8 0.88081E-08 0.18550E+07 0.35847E+02 c k 0.24521E+04 1 0.12573E-05 0.77775E+05 0.14142E+04 c omega 0.81514E+09 1 0.42737E-08 0.33253E+12 0.42226E+02 c TotEner 0.24216E+06 1 0.11247E-05 0.44715E+07 0.23022E+02 c temperature 0.00000E+00 0 0.00000E+00 0.80194E+01 0.22845E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9979e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.28 226.28 0.0017418 0.00089764 v Velocity[Y] -0.13017 701.9 250.51 80.992 v Velocity[Z] -19.204 359.25 24.925 1.9599 v ǁVelocityǁ 0.12453 701.9 260.07 83.733 v Pressure 50675 1.1024e+05 1.0358e+05 1.0416e+05 v k 1.18e-08 41697 910.03 355.43 v omega 154.14 9.6783e+09 1.8459e+08 3.4143e+05 v TotEner 93644 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 65.657 533.95 397.95 337.19 v Density 0.39382 4.6838 0.94919 1.0903 v TurbVisc 8.787e-19 0.06412 0.010066 0.028636 v CourantNb 1.3098e-05 43.21 0.3894 0.007592 v FourierNb 4.5069e-05 208.21 1.8446 0.090603 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 65.733 533.95 402.96 421.94 v Boundary Density 0.39393 4.6795 0.98704 0.89808 v Yplus 0 44.398 2.4483 0.95508 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8328e-05 43.92 0.47949 0.010617 INSTANT 0.158993563E-01 TIME STEP NUMBER 30123 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.654611163E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560859503E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123312300E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10344E+01 0.58030E+02 Friction velocity uk : 0.10344E+01 0.58030E+02 Dimensionless distance yplus : 0.20562E-01 0.44418E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14441E-01 0.12503E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60109E+03 2 0.24650E-06 0.41358E+02 0.15536E+03 c Velocity[X] 0.17473E+01 c Velocity[Y] 0.10970E+02 c Velocity[Z] 0.28641E+02 c Pressure 0.75756E-01 8 0.90757E-08 0.18623E+07 0.35918E+02 c k 0.24524E+04 1 0.12607E-05 0.77966E+05 0.14158E+04 c omega 0.81514E+09 1 0.42701E-08 0.31639E+12 0.41188E+02 c TotEner 0.24216E+06 1 0.11243E-05 0.44866E+07 0.23061E+02 c temperature 0.00000E+00 0 0.00000E+00 0.80454E+01 0.22882E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9974e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.31 226.31 0.0017439 0.00090096 v Velocity[Y] -0.13017 701.9 250.51 80.993 v Velocity[Z] -19.203 359.38 24.93 1.9601 v ǁVelocityǁ 0.12796 701.9 260.07 83.733 v Pressure 50658 1.1024e+05 1.0357e+05 1.0416e+05 v k 1.1799e-08 41714 910.06 355.43 v omega 154.15 9.6783e+09 1.8459e+08 3.4143e+05 v TotEner 93589 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 65.581 533.95 397.95 337.19 v Density 0.39371 4.6881 0.94919 1.0903 v TurbVisc 8.7866e-19 0.06412 0.010066 0.028637 v CourantNb 1.3101e-05 43.219 0.38947 0.0075921 v FourierNb 4.5069e-05 208.13 1.8443 0.090605 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 65.657 533.95 402.96 421.94 v Boundary Density 0.39382 4.6838 0.9871 0.89809 v Yplus 0 44.418 2.4483 0.95514 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8332e-05 43.928 0.47957 0.010617 INSTANT 0.158996193E-01 TIME STEP NUMBER 30124 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.654222424E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560867594E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123358616E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10344E+01 0.58034E+02 Friction velocity uk : 0.10344E+01 0.58034E+02 Dimensionless distance yplus : 0.20561E-01 0.44438E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14441E-01 0.12504E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60109E+03 2 0.24637E-06 0.41362E+02 0.15536E+03 c Velocity[X] 0.17287E+01 c Velocity[Y] 0.10970E+02 c Velocity[Z] 0.28664E+02 c Pressure 0.75760E-01 8 0.91507E-08 0.18700E+07 0.35992E+02 c k 0.24526E+04 1 0.12642E-05 0.78138E+05 0.14172E+04 c omega 0.81514E+09 1 0.46173E-08 0.36089E+12 0.43989E+02 c TotEner 0.24216E+06 1 0.11239E-05 0.44983E+07 0.23091E+02 c temperature 0.00000E+00 0 0.00000E+00 0.80714E+01 0.22919E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9968e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.34 226.34 0.0017459 0.00090426 v Velocity[Y] -0.13016 701.9 250.51 80.993 v Velocity[Z] -19.203 359.51 24.935 1.9603 v ǁVelocityǁ 0.13143 701.9 260.08 83.734 v Pressure 50641 1.1024e+05 1.0357e+05 1.0416e+05 v k 1.1799e-08 41731 910.1 355.43 v omega 154.15 9.6783e+09 1.8459e+08 3.4143e+05 v TotEner 93533 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 65.504 533.95 397.95 337.19 v Density 0.3936 4.6925 0.94918 1.0903 v TurbVisc 8.7863e-19 0.06412 0.010066 0.028637 v CourantNb 1.3104e-05 43.227 0.38954 0.0075922 v FourierNb 4.5069e-05 208.04 1.8439 0.090606 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 65.581 533.95 402.95 421.94 v Boundary Density 0.39371 4.6881 0.98716 0.8981 v Yplus 0 44.438 2.4484 0.9552 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8336e-05 43.936 0.47964 0.010618 INSTANT 0.158998823E-01 TIME STEP NUMBER 30125 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.653808982E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560875600E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123403731E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10344E+01 0.58038E+02 Friction velocity uk : 0.10344E+01 0.58038E+02 Dimensionless distance yplus : 0.20561E-01 0.44459E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14441E-01 0.12505E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60109E+03 2 0.24624E-06 0.41369E+02 0.15538E+03 c Velocity[X] 0.17105E+01 c Velocity[Y] 0.10967E+02 c Velocity[Z] 0.28691E+02 c Pressure 0.75764E-01 8 0.91710E-08 0.18778E+07 0.36067E+02 c k 0.24529E+04 1 0.12678E-05 0.78311E+05 0.14187E+04 c omega 0.81514E+09 1 0.42882E-08 0.36795E+12 0.44418E+02 c TotEner 0.24216E+06 1 0.11234E-05 0.45095E+07 0.23120E+02 c temperature 0.00000E+00 0 0.00000E+00 0.80974E+01 0.22956E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9963e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.37 226.37 0.0017481 0.00090756 v Velocity[Y] -0.13016 701.9 250.51 80.994 v Velocity[Z] -19.202 359.63 24.94 1.9605 v ǁVelocityǁ 0.13491 701.9 260.08 83.735 v Pressure 50624 1.1024e+05 1.0357e+05 1.0416e+05 v k 1.1798e-08 41748 910.13 355.43 v omega 154.16 9.6783e+09 1.8459e+08 3.4143e+05 v TotEner 93478 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 65.427 533.95 397.95 337.19 v Density 0.39349 4.6969 0.94918 1.0903 v TurbVisc 8.786e-19 0.06412 0.010066 0.028637 v CourantNb 1.3106e-05 43.236 0.38962 0.0075924 v FourierNb 4.507e-05 207.96 1.8436 0.090607 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 65.504 533.95 402.95 421.94 v Boundary Density 0.3936 4.6925 0.98722 0.89811 v Yplus 0 44.459 2.4484 0.95527 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8339e-05 43.944 0.47972 0.010618 INSTANT 0.159001453E-01 TIME STEP NUMBER 30126 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.653371904E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560883510E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123447638E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10344E+01 0.58042E+02 Friction velocity uk : 0.10344E+01 0.58042E+02 Dimensionless distance yplus : 0.20561E-01 0.44480E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14441E-01 0.12506E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60109E+03 2 0.24612E-06 0.41371E+02 0.15538E+03 c Velocity[X] 0.16926E+01 c Velocity[Y] 0.10956E+02 c Velocity[Z] 0.28723E+02 c Pressure 0.75768E-01 8 0.91116E-08 0.18861E+07 0.36146E+02 c k 0.24532E+04 1 0.12720E-05 0.78494E+05 0.14203E+04 c omega 0.81514E+09 1 0.40098E-08 0.31984E+12 0.41412E+02 c TotEner 0.24216E+06 1 0.11230E-05 0.45189E+07 0.23144E+02 c temperature 0.00000E+00 0 0.00000E+00 0.81240E+01 0.22993E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9958e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.4 226.4 0.0017502 0.00091085 v Velocity[Y] -0.13016 701.9 250.51 80.995 v Velocity[Z] -19.202 359.76 24.945 1.9607 v ǁVelocityǁ 0.13842 701.9 260.08 83.736 v Pressure 50607 1.1024e+05 1.0357e+05 1.0416e+05 v k 1.1798e-08 41765 910.17 355.43 v omega 154.16 9.6783e+09 1.8459e+08 3.4143e+05 v TotEner 93422 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 65.349 533.95 397.95 337.19 v Density 0.39338 4.7012 0.94918 1.0903 v TurbVisc 8.7857e-19 0.064119 0.010066 0.028637 v CourantNb 1.3109e-05 43.244 0.38969 0.0075925 v FourierNb 4.507e-05 207.87 1.8433 0.090608 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 65.427 533.95 402.94 421.94 v Boundary Density 0.39349 4.6969 0.98728 0.89813 v Yplus 0 44.48 2.4484 0.95533 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8343e-05 43.952 0.47979 0.010618 INSTANT 0.159004083E-01 TIME STEP NUMBER 30127 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.652912284E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560891310E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123490338E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10344E+01 0.58046E+02 Friction velocity uk : 0.10344E+01 0.58046E+02 Dimensionless distance yplus : 0.20561E-01 0.44500E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14440E-01 0.12508E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60110E+03 2 0.24599E-06 0.41390E+02 0.15541E+03 c Velocity[X] 0.16752E+01 c Velocity[Y] 0.10956E+02 c Velocity[Z] 0.28759E+02 c Pressure 0.75772E-01 8 0.90015E-08 0.18944E+07 0.36226E+02 c k 0.24535E+04 1 0.12772E-05 0.78742E+05 0.14224E+04 c omega 0.81514E+09 1 0.50975E-08 0.51648E+12 0.52624E+02 c TotEner 0.24217E+06 1 0.11225E-05 0.45312E+07 0.23175E+02 c temperature 0.00000E+00 0 0.00000E+00 0.81522E+01 0.23033E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9952e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.43 226.43 0.0017525 0.00091414 v Velocity[Y] -0.13015 701.9 250.51 80.996 v Velocity[Z] -19.201 359.89 24.95 1.9609 v ǁVelocityǁ 0.14194 701.9 260.09 83.737 v Pressure 50591 1.1024e+05 1.0357e+05 1.0416e+05 v k 1.1798e-08 41782 910.2 355.43 v omega 154.17 9.6783e+09 1.8459e+08 3.4144e+05 v TotEner 93365 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 65.271 533.95 397.94 337.19 v Density 0.39327 4.7056 0.94917 1.0903 v TurbVisc 8.7853e-19 0.064119 0.010066 0.028637 v CourantNb 1.3111e-05 43.253 0.38976 0.0075927 v FourierNb 4.507e-05 207.79 1.843 0.09061 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 65.349 533.95 402.94 421.94 v Boundary Density 0.39338 4.7012 0.98734 0.89814 v Yplus 0 44.5 2.4484 0.95539 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8346e-05 43.96 0.47986 0.010618 INSTANT 0.159006713E-01 TIME STEP NUMBER 30128 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.652431240E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560898978E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123531835E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10343E+01 0.58050E+02 Friction velocity uk : 0.10343E+01 0.58050E+02 Dimensionless distance yplus : 0.20560E-01 0.44521E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14440E-01 0.12509E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60110E+03 2 0.24587E-06 0.41418E+02 0.15546E+03 c Velocity[X] 0.16582E+01 c Velocity[Y] 0.10961E+02 c Velocity[Z] 0.28799E+02 c Pressure 0.75776E-01 8 0.90971E-08 0.19033E+07 0.36311E+02 c k 0.24538E+04 1 0.12826E-05 0.78989E+05 0.14245E+04 c omega 0.81514E+09 1 0.52084E-08 0.47755E+12 0.50602E+02 c TotEner 0.24217E+06 1 0.11221E-05 0.45451E+07 0.23211E+02 c temperature 0.00000E+00 0 0.00000E+00 0.81821E+01 0.23076E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9947e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.46 226.46 0.0017546 0.00091742 v Velocity[Y] -0.13015 701.9 250.51 80.997 v Velocity[Z] -19.201 360.01 24.955 1.961 v ǁVelocityǁ 0.14549 701.9 260.09 83.738 v Pressure 50574 1.1024e+05 1.0357e+05 1.0416e+05 v k 1.1797e-08 41798 910.23 355.43 v omega 154.17 9.6783e+09 1.8459e+08 3.4144e+05 v TotEner 93308 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 65.193 533.95 397.94 337.19 v Density 0.39316 4.7101 0.94917 1.0903 v TurbVisc 8.785e-19 0.064119 0.010066 0.028637 v CourantNb 1.3114e-05 43.261 0.38983 0.0075928 v FourierNb 4.507e-05 207.71 1.8427 0.090611 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 65.271 533.95 402.93 421.93 v Boundary Density 0.39327 4.7056 0.9874 0.89815 v Yplus 0 44.521 2.4485 0.95545 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.835e-05 43.968 0.47994 0.010618 INSTANT 0.159009343E-01 TIME STEP NUMBER 30129 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.651929910E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560906495E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123572140E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10343E+01 0.58054E+02 Friction velocity uk : 0.10343E+01 0.58054E+02 Dimensionless distance yplus : 0.20560E-01 0.44542E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14440E-01 0.12510E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60110E+03 2 0.24574E-06 0.41451E+02 0.15552E+03 c Velocity[X] 0.16416E+01 c Velocity[Y] 0.10966E+02 c Velocity[Z] 0.28843E+02 c Pressure 0.75780E-01 8 0.92732E-08 0.19121E+07 0.36395E+02 c k 0.24540E+04 1 0.12886E-05 0.79293E+05 0.14271E+04 c omega 0.81514E+09 1 0.52896E-08 0.45503E+12 0.49394E+02 c TotEner 0.24217E+06 1 0.11217E-05 0.45585E+07 0.23245E+02 c temperature 0.00000E+00 0 0.00000E+00 0.82124E+01 0.23118E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9942e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.48 226.49 0.0017568 0.0009207 v Velocity[Y] -0.13015 701.9 250.51 80.998 v Velocity[Z] -19.2 360.14 24.959 1.9612 v ǁVelocityǁ 0.14906 701.9 260.1 83.739 v Pressure 50558 1.1024e+05 1.0357e+05 1.0416e+05 v k 1.1797e-08 41815 910.27 355.43 v omega 154.18 9.6783e+09 1.8459e+08 3.4144e+05 v TotEner 93251 6.2951e+05 3.4159e+05 2.4853e+05 v temperature 65.114 533.95 397.94 337.19 v Density 0.39305 4.7145 0.94916 1.0903 v TurbVisc 8.7847e-19 0.064119 0.010066 0.028637 v CourantNb 1.3116e-05 43.27 0.3899 0.0075929 v FourierNb 4.507e-05 207.63 1.8424 0.090612 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 65.193 533.95 402.93 421.93 v Boundary Density 0.39316 4.7101 0.98746 0.89816 v Yplus 0 44.542 2.4485 0.95552 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8353e-05 43.975 0.48001 0.010619 INSTANT 0.159011973E-01 TIME STEP NUMBER 30130 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.651409456E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560913844E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123611266E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10343E+01 0.58058E+02 Friction velocity uk : 0.10343E+01 0.58058E+02 Dimensionless distance yplus : 0.20560E-01 0.44563E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14440E-01 0.12511E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60110E+03 2 0.24562E-06 0.41496E+02 0.15561E+03 c Velocity[X] 0.16253E+01 c Velocity[Y] 0.10979E+02 c Velocity[Z] 0.28892E+02 c Pressure 0.75784E-01 8 0.93643E-08 0.19213E+07 0.36482E+02 c k 0.24543E+04 1 0.12958E-05 0.79660E+05 0.14303E+04 c omega 0.81515E+09 1 0.55219E-08 0.49274E+12 0.51400E+02 c TotEner 0.24217E+06 1 0.11213E-05 0.45745E+07 0.23286E+02 c temperature 0.00000E+00 0 0.00000E+00 0.82446E+01 0.23163E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9937e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.51 226.51 0.0017588 0.00092397 v Velocity[Y] -0.13014 701.9 250.51 80.999 v Velocity[Z] -19.2 360.27 24.964 1.9614 v ǁVelocityǁ 0.15265 701.9 260.1 83.74 v Pressure 50541 1.1024e+05 1.0357e+05 1.0416e+05 v k 1.1796e-08 41832 910.3 355.42 v omega 154.18 9.6783e+09 1.8459e+08 3.4144e+05 v TotEner 93194 6.2951e+05 3.416e+05 2.4853e+05 v temperature 65.034 533.95 397.94 337.19 v Density 0.39294 4.719 0.94916 1.0903 v TurbVisc 8.7844e-19 0.064119 0.010066 0.028638 v CourantNb 1.3118e-05 43.278 0.38997 0.0075931 v FourierNb 4.5071e-05 207.55 1.8421 0.090613 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 65.114 533.95 402.92 421.93 v Boundary Density 0.39305 4.7145 0.98752 0.89818 v Yplus 0 44.563 2.4485 0.95558 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8356e-05 43.983 0.48008 0.010619 INSTANT 0.159014603E-01 TIME STEP NUMBER 30131 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.650871058E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560921016E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123649228E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10343E+01 0.58062E+02 Friction velocity uk : 0.10343E+01 0.58062E+02 Dimensionless distance yplus : 0.20560E-01 0.44584E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14440E-01 0.12512E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60110E+03 2 0.24549E-06 0.41554E+02 0.15572E+03 c Velocity[X] 0.16094E+01 c Velocity[Y] 0.11001E+02 c Velocity[Z] 0.28944E+02 c Pressure 0.75788E-01 8 0.95773E-08 0.19308E+07 0.36573E+02 c k 0.24546E+04 1 0.13027E-05 0.79986E+05 0.14332E+04 c omega 0.81515E+09 1 0.48305E-08 0.40718E+12 0.46725E+02 c TotEner 0.24217E+06 1 0.11209E-05 0.45931E+07 0.23333E+02 c temperature 0.00000E+00 0 0.00000E+00 0.82788E+01 0.23211E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9932e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.54 226.54 0.0017608 0.00092723 v Velocity[Y] -0.13014 701.9 250.52 81 v Velocity[Z] -19.199 360.39 24.969 1.9616 v ǁVelocityǁ 0.15626 701.9 260.1 83.741 v Pressure 50525 1.1024e+05 1.0357e+05 1.0416e+05 v k 1.1796e-08 41849 910.33 355.42 v omega 154.19 9.6783e+09 1.8459e+08 3.4144e+05 v TotEner 93136 6.2951e+05 3.416e+05 2.4853e+05 v temperature 64.954 533.95 397.94 337.19 v Density 0.39284 4.7234 0.94916 1.0903 v TurbVisc 8.784e-19 0.064119 0.010067 0.028638 v CourantNb 1.3121e-05 43.287 0.39004 0.0075932 v FourierNb 4.5071e-05 207.48 1.8419 0.090615 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 65.034 533.95 402.92 421.93 v Boundary Density 0.39294 4.719 0.98758 0.89819 v Yplus 0 44.584 2.4486 0.95564 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8359e-05 43.99 0.48016 0.010619 INSTANT 0.159017233E-01 TIME STEP NUMBER 30132 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.650315913E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560928001E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123686046E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10343E+01 0.58066E+02 Friction velocity uk : 0.10343E+01 0.58066E+02 Dimensionless distance yplus : 0.20559E-01 0.44605E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14440E-01 0.12513E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60110E+03 2 0.24537E-06 0.41572E+02 0.15575E+03 c Velocity[X] 0.15938E+01 c Velocity[Y] 0.10978E+02 c Velocity[Z] 0.29000E+02 c Pressure 0.75792E-01 9 0.86954E-08 0.19404E+07 0.36663E+02 c k 0.24549E+04 1 0.13094E-05 0.80230E+05 0.14352E+04 c omega 0.81515E+09 1 0.45898E-08 0.35592E+12 0.43685E+02 c TotEner 0.24217E+06 1 0.11204E-05 0.45983E+07 0.23346E+02 c temperature 0.00000E+00 0 0.00000E+00 0.83094E+01 0.23254E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9926e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.57 226.57 0.0017627 0.00093049 v Velocity[Y] -0.13013 701.9 250.52 81.001 v Velocity[Z] -19.199 360.52 24.974 1.9618 v ǁVelocityǁ 0.15989 701.9 260.11 83.742 v Pressure 50508 1.1024e+05 1.0357e+05 1.0416e+05 v k 1.1795e-08 41866 910.37 355.42 v omega 154.19 9.6783e+09 1.8459e+08 3.4144e+05 v TotEner 93078 6.2951e+05 3.416e+05 2.4853e+05 v temperature 64.874 533.95 397.94 337.19 v Density 0.39273 4.7279 0.94915 1.0903 v TurbVisc 8.7837e-19 0.064119 0.010067 0.028638 v CourantNb 1.3123e-05 43.295 0.39011 0.0075934 v FourierNb 4.5071e-05 207.4 1.8416 0.090616 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 64.954 533.95 402.91 421.93 v Boundary Density 0.39284 4.7234 0.98764 0.8982 v Yplus 0 44.605 2.4486 0.95571 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8363e-05 43.998 0.48023 0.010619 INSTANT 0.159019864E-01 TIME STEP NUMBER 30133 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.649745236E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560934785E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123721740E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10343E+01 0.58069E+02 Friction velocity uk : 0.10343E+01 0.58069E+02 Dimensionless distance yplus : 0.20559E-01 0.44626E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14439E-01 0.12514E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60111E+03 2 0.24524E-06 0.41612E+02 0.15582E+03 c Velocity[X] 0.15786E+01 c Velocity[Y] 0.10973E+02 c Velocity[Z] 0.29060E+02 c Pressure 0.75796E-01 8 0.93094E-08 0.19501E+07 0.36755E+02 c k 0.24552E+04 1 0.13167E-05 0.80524E+05 0.14377E+04 c omega 0.81515E+09 1 0.43107E-08 0.28982E+12 0.39420E+02 c TotEner 0.24217E+06 1 0.11200E-05 0.46089E+07 0.23373E+02 c temperature 0.00000E+00 0 0.00000E+00 0.83434E+01 0.23302E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9921e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.6 226.6 0.0017647 0.00093375 v Velocity[Y] -0.13013 701.9 250.52 81.002 v Velocity[Z] -19.198 360.64 24.979 1.962 v ǁVelocityǁ 0.16354 701.9 260.11 83.743 v Pressure 50492 1.1024e+05 1.0356e+05 1.0416e+05 v k 1.1795e-08 41883 910.4 355.42 v omega 154.2 9.6783e+09 1.8459e+08 3.4144e+05 v TotEner 93020 6.2951e+05 3.416e+05 2.4853e+05 v temperature 64.794 533.95 397.94 337.19 v Density 0.39262 4.7325 0.94915 1.0903 v TurbVisc 8.7834e-19 0.064119 0.010067 0.028638 v CourantNb 1.3125e-05 43.304 0.39018 0.0075935 v FourierNb 4.5072e-05 207.33 1.8413 0.090617 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 64.874 533.95 402.91 421.93 v Boundary Density 0.39273 4.7279 0.9877 0.89821 v Yplus 0 44.626 2.4486 0.95577 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8366e-05 44.005 0.4803 0.010619 INSTANT 0.159022494E-01 TIME STEP NUMBER 30134 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.649160255E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560941346E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123756335E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10343E+01 0.58073E+02 Friction velocity uk : 0.10343E+01 0.58073E+02 Dimensionless distance yplus : 0.20559E-01 0.44647E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14439E-01 0.12515E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60111E+03 2 0.24511E-06 0.41659E+02 0.15591E+03 c Velocity[X] 0.15638E+01 c Velocity[Y] 0.10971E+02 c Velocity[Z] 0.29125E+02 c Pressure 0.75800E-01 8 0.90561E-08 0.19601E+07 0.36849E+02 c k 0.24554E+04 1 0.13243E-05 0.80860E+05 0.14406E+04 c omega 0.81515E+09 1 0.44481E-08 0.31127E+12 0.40853E+02 c TotEner 0.24218E+06 1 0.11196E-05 0.46206E+07 0.23402E+02 c temperature 0.00000E+00 0 0.00000E+00 0.83786E+01 0.23351E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9916e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.63 226.63 0.0017666 0.000937 v Velocity[Y] -0.13013 701.9 250.52 81.003 v Velocity[Z] -19.198 360.77 24.984 1.9622 v ǁVelocityǁ 0.1672 701.9 260.11 83.744 v Pressure 50475 1.1024e+05 1.0356e+05 1.0416e+05 v k 1.1795e-08 41900 910.43 355.42 v omega 154.2 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92962 6.2951e+05 3.416e+05 2.4853e+05 v temperature 64.713 533.95 397.94 337.19 v Density 0.39251 4.737 0.94914 1.0903 v TurbVisc 8.7831e-19 0.064118 0.010067 0.028638 v CourantNb 1.3127e-05 43.312 0.39025 0.0075936 v FourierNb 4.5072e-05 207.26 1.841 0.090618 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 64.794 533.95 402.9 421.93 v Boundary Density 0.39262 4.7325 0.98776 0.89823 v Yplus 0 44.647 2.4487 0.95584 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8369e-05 44.013 0.48037 0.010619 INSTANT 0.159025124E-01 TIME STEP NUMBER 30135 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.648562220E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560947676E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123789853E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10343E+01 0.58077E+02 Friction velocity uk : 0.10343E+01 0.58077E+02 Dimensionless distance yplus : 0.20559E-01 0.44669E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14439E-01 0.12517E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60111E+03 2 0.24499E-06 0.41682E+02 0.15595E+03 c Velocity[X] 0.15493E+01 c Velocity[Y] 0.10941E+02 c Velocity[Z] 0.29192E+02 c Pressure 0.75804E-01 8 0.89918E-08 0.19706E+07 0.36947E+02 c k 0.24557E+04 1 0.13309E-05 0.81132E+05 0.14429E+04 c omega 0.81515E+09 1 0.42186E-08 0.28052E+12 0.38783E+02 c TotEner 0.24218E+06 1 0.11190E-05 0.46252E+07 0.23414E+02 c temperature 0.00000E+00 0 0.00000E+00 0.84132E+01 0.23399E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9911e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.66 226.66 0.0017685 0.00094024 v Velocity[Y] -0.13012 701.9 250.52 81.004 v Velocity[Z] -19.197 360.89 24.989 1.9623 v ǁVelocityǁ 0.17088 701.9 260.12 83.744 v Pressure 50459 1.1024e+05 1.0356e+05 1.0416e+05 v k 1.1794e-08 41917 910.47 355.42 v omega 154.21 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92903 6.2951e+05 3.416e+05 2.4853e+05 v temperature 64.631 533.95 397.93 337.19 v Density 0.39241 4.7416 0.94914 1.0903 v TurbVisc 8.7827e-19 0.064118 0.010067 0.028638 v CourantNb 1.3129e-05 43.32 0.39032 0.0075938 v FourierNb 4.5072e-05 207.18 1.8407 0.09062 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 64.713 533.95 402.9 421.93 v Boundary Density 0.39251 4.737 0.98782 0.89824 v Yplus 0 44.669 2.4487 0.9559 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8372e-05 44.02 0.48044 0.01062 INSTANT 0.159027754E-01 TIME STEP NUMBER 30136 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.647952381E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560953751E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123822322E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10343E+01 0.58081E+02 Friction velocity uk : 0.10343E+01 0.58081E+02 Dimensionless distance yplus : 0.20558E-01 0.44690E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14439E-01 0.12518E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60111E+03 2 0.24486E-06 0.41733E+02 0.15604E+03 c Velocity[X] 0.15351E+01 c Velocity[Y] 0.10933E+02 c Velocity[Z] 0.29265E+02 c Pressure 0.75808E-01 8 0.90912E-08 0.19811E+07 0.37046E+02 c k 0.24560E+04 1 0.13390E-05 0.81486E+05 0.14460E+04 c omega 0.81515E+09 1 0.40747E-08 0.26899E+12 0.37978E+02 c TotEner 0.24218E+06 1 0.11186E-05 0.46362E+07 0.23442E+02 c temperature 0.00000E+00 0 0.00000E+00 0.84510E+01 0.23451E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9906e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.68 226.68 0.0017702 0.00094347 v Velocity[Y] -0.13012 701.9 250.52 81.005 v Velocity[Z] -19.197 361.02 24.994 1.9625 v ǁVelocityǁ 0.17458 701.9 260.12 83.745 v Pressure 50443 1.1024e+05 1.0356e+05 1.0416e+05 v k 1.1794e-08 41934 910.5 355.42 v omega 154.21 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92844 6.2951e+05 3.416e+05 2.4853e+05 v temperature 64.55 533.95 397.93 337.19 v Density 0.3923 4.7462 0.94914 1.0903 v TurbVisc 8.7824e-19 0.064118 0.010067 0.028639 v CourantNb 1.3131e-05 43.329 0.39039 0.0075939 v FourierNb 4.5073e-05 207.11 1.8405 0.090621 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 64.631 533.95 402.89 421.93 v Boundary Density 0.39241 4.7416 0.98788 0.89825 v Yplus 0 44.69 2.4487 0.95597 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8375e-05 44.028 0.48052 0.01062 INSTANT 0.159030384E-01 TIME STEP NUMBER 30137 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.647332002E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560959558E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123853766E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10342E+01 0.58085E+02 Friction velocity uk : 0.10342E+01 0.58085E+02 Dimensionless distance yplus : 0.20558E-01 0.44712E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14439E-01 0.12519E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60111E+03 2 0.24474E-06 0.41790E+02 0.15615E+03 c Velocity[X] 0.15213E+01 c Velocity[Y] 0.10927E+02 c Velocity[Z] 0.29341E+02 c Pressure 0.75812E-01 8 0.91431E-08 0.19920E+07 0.37148E+02 c k 0.24563E+04 1 0.13477E-05 0.81868E+05 0.14492E+04 c omega 0.81515E+09 1 0.37176E-08 0.23423E+12 0.35438E+02 c TotEner 0.24218E+06 1 0.11182E-05 0.46474E+07 0.23470E+02 c temperature 0.00000E+00 0 0.00000E+00 0.84901E+01 0.23506E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9901e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.71 226.71 0.0017719 0.0009467 v Velocity[Y] -0.13012 701.9 250.52 81.006 v Velocity[Z] -19.196 361.14 24.999 1.9627 v ǁVelocityǁ 0.1783 701.9 260.13 83.746 v Pressure 50427 1.1024e+05 1.0356e+05 1.0416e+05 v k 1.1793e-08 41951 910.53 355.42 v omega 154.22 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92784 6.2951e+05 3.416e+05 2.4853e+05 v temperature 64.467 533.95 397.93 337.19 v Density 0.39219 4.7508 0.94913 1.0903 v TurbVisc 8.7821e-19 0.064118 0.010067 0.028639 v CourantNb 1.3133e-05 43.337 0.39046 0.007594 v FourierNb 4.5073e-05 207.04 1.8402 0.090622 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 64.55 533.95 402.89 421.93 v Boundary Density 0.3923 4.7462 0.98794 0.89826 v Yplus 0 44.712 2.4488 0.95603 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8378e-05 44.035 0.48059 0.01062 INSTANT 0.159033014E-01 TIME STEP NUMBER 30138 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.646702360E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560965086E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123884214E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10342E+01 0.58088E+02 Friction velocity uk : 0.10342E+01 0.58088E+02 Dimensionless distance yplus : 0.20558E-01 0.44733E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14439E-01 0.12520E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60111E+03 2 0.24461E-06 0.41864E+02 0.15629E+03 c Velocity[X] 0.15077E+01 c Velocity[Y] 0.10934E+02 c Velocity[Z] 0.29422E+02 c Pressure 0.75816E-01 8 0.88576E-08 0.20031E+07 0.37251E+02 c k 0.24566E+04 1 0.13572E-05 0.82304E+05 0.14530E+04 c omega 0.81515E+09 1 0.44774E-08 0.32840E+12 0.41962E+02 c TotEner 0.24218E+06 1 0.11178E-05 0.46617E+07 0.23506E+02 c temperature 0.00000E+00 0 0.00000E+00 0.85312E+01 0.23562E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9896e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.74 226.74 0.0017735 0.00094993 v Velocity[Y] -0.13011 701.9 250.52 81.007 v Velocity[Z] -19.195 361.27 25.003 1.9629 v ǁVelocityǁ 0.18203 701.9 260.13 83.747 v Pressure 50410 1.1024e+05 1.0356e+05 1.0416e+05 v k 1.1793e-08 41968 910.57 355.42 v omega 154.22 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92724 6.2951e+05 3.416e+05 2.4853e+05 v temperature 64.385 533.95 397.93 337.19 v Density 0.39209 4.7555 0.94913 1.0903 v TurbVisc 8.7818e-19 0.064118 0.010067 0.028639 v CourantNb 1.3135e-05 43.345 0.39052 0.0075942 v FourierNb 4.5074e-05 206.97 1.84 0.090623 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 64.467 533.95 402.88 421.92 v Boundary Density 0.39219 4.7508 0.988 0.89828 v Yplus 0 44.733 2.4488 0.9561 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.838e-05 44.042 0.48066 0.01062 INSTANT 0.159035644E-01 TIME STEP NUMBER 30139 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.646064740E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560970326E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123913692E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10342E+01 0.58092E+02 Friction velocity uk : 0.10342E+01 0.58092E+02 Dimensionless distance yplus : 0.20558E-01 0.44755E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14438E-01 0.12521E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60112E+03 2 0.24449E-06 0.41934E+02 0.15641E+03 c Velocity[X] 0.14946E+01 c Velocity[Y] 0.10933E+02 c Velocity[Z] 0.29507E+02 c Pressure 0.75820E-01 8 0.85565E-08 0.20147E+07 0.37359E+02 c k 0.24569E+04 1 0.13664E-05 0.82715E+05 0.14565E+04 c omega 0.81515E+09 1 0.43745E-08 0.31662E+12 0.41202E+02 c TotEner 0.24218E+06 1 0.11174E-05 0.46747E+07 0.23539E+02 c temperature 0.00000E+00 0 0.00000E+00 0.85736E+01 0.23621E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9891e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.77 226.77 0.001775 0.00095315 v Velocity[Y] -0.13011 701.9 250.52 81.008 v Velocity[Z] -19.195 361.39 25.008 1.9631 v ǁVelocityǁ 0.18578 701.9 260.13 83.748 v Pressure 50394 1.1024e+05 1.0356e+05 1.0416e+05 v k 1.1793e-08 41986 910.6 355.42 v omega 154.23 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92664 6.2951e+05 3.416e+05 2.4853e+05 v temperature 64.302 533.95 397.93 337.19 v Density 0.39198 4.7601 0.94912 1.0903 v TurbVisc 8.7815e-19 0.064118 0.010068 0.028639 v CourantNb 1.3137e-05 43.353 0.39059 0.0075943 v FourierNb 4.5074e-05 206.91 1.8397 0.090625 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 64.385 533.95 402.87 421.92 v Boundary Density 0.39209 4.7555 0.98806 0.89829 v Yplus 0 44.755 2.4488 0.95617 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8383e-05 44.05 0.48073 0.01062 INSTANT 0.159038274E-01 TIME STEP NUMBER 30140 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.645420434E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560975272E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123942227E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10342E+01 0.58096E+02 Friction velocity uk : 0.10342E+01 0.58096E+02 Dimensionless distance yplus : 0.20558E-01 0.44777E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14438E-01 0.12522E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60112E+03 2 0.24437E-06 0.42003E+02 0.15654E+03 c Velocity[X] 0.14817E+01 c Velocity[Y] 0.10926E+02 c Velocity[Z] 0.29595E+02 c Pressure 0.75824E-01 5 0.99284E-08 0.20265E+07 0.37468E+02 c k 0.24572E+04 1 0.13762E-05 0.83158E+05 0.14603E+04 c omega 0.81515E+09 1 0.48365E-08 0.49948E+12 0.51750E+02 c TotEner 0.24218E+06 1 0.11170E-05 0.46861E+07 0.23568E+02 c temperature 0.00000E+00 0 0.00000E+00 0.86167E+01 0.23680E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9886e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.8 226.8 0.0017764 0.00095636 v Velocity[Y] -0.13011 701.9 250.52 81.009 v Velocity[Z] -19.194 361.52 25.013 1.9633 v ǁVelocityǁ 0.18954 701.9 260.14 83.749 v Pressure 50378 1.1024e+05 1.0356e+05 1.0416e+05 v k 1.1792e-08 42003 910.64 355.42 v omega 154.23 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92604 6.2951e+05 3.416e+05 2.4854e+05 v temperature 64.219 533.95 397.93 337.19 v Density 0.39187 4.7649 0.94912 1.0903 v TurbVisc 8.7812e-19 0.064118 0.010068 0.028639 v CourantNb 1.3139e-05 43.362 0.39066 0.0075945 v FourierNb 4.5075e-05 206.84 1.8394 0.090626 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 64.302 533.95 402.87 421.92 v Boundary Density 0.39198 4.7601 0.98813 0.8983 v Yplus 0 44.777 2.4489 0.95624 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8386e-05 44.057 0.4808 0.010621 INSTANT 0.159040904E-01 TIME STEP NUMBER 30141 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.644770740E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560979908E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123969845E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10342E+01 0.58100E+02 Friction velocity uk : 0.10342E+01 0.58100E+02 Dimensionless distance yplus : 0.20557E-01 0.44799E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14438E-01 0.12523E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60112E+03 2 0.24424E-06 0.42097E+02 0.15672E+03 c Velocity[X] 0.14691E+01 c Velocity[Y] 0.10939E+02 c Velocity[Z] 0.29689E+02 c Pressure 0.75828E-01 5 0.96904E-08 0.20387E+07 0.37581E+02 c k 0.24575E+04 1 0.13868E-05 0.83675E+05 0.14647E+04 c omega 0.81515E+09 1 0.45013E-08 0.41478E+12 0.47159E+02 c TotEner 0.24219E+06 1 0.11166E-05 0.47036E+07 0.23611E+02 c temperature 0.00000E+00 0 0.00000E+00 0.86632E+01 0.23744E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9881e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.82 226.82 0.0017778 0.00095957 v Velocity[Y] -0.1301 701.9 250.52 81.01 v Velocity[Z] -19.194 361.64 25.018 1.9635 v ǁVelocityǁ 0.19331 701.9 260.14 83.75 v Pressure 50362 1.1024e+05 1.0356e+05 1.0416e+05 v k 1.1792e-08 42020 910.67 355.41 v omega 154.24 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92543 6.2951e+05 3.416e+05 2.4854e+05 v temperature 64.135 533.95 397.93 337.2 v Density 0.39177 4.7696 0.94912 1.0903 v TurbVisc 8.7808e-19 0.064118 0.010068 0.028639 v CourantNb 1.3141e-05 43.37 0.39073 0.0075946 v FourierNb 4.5075e-05 206.77 1.8392 0.090627 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 64.219 533.95 402.86 421.92 v Boundary Density 0.39187 4.7649 0.98819 0.89832 v Yplus 0 44.799 2.4489 0.9563 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8389e-05 44.064 0.48087 0.010621 INSTANT 0.159043534E-01 TIME STEP NUMBER 30142 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.644116960E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560984231E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123996574E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10342E+01 0.58103E+02 Friction velocity uk : 0.10342E+01 0.58103E+02 Dimensionless distance yplus : 0.20557E-01 0.44821E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14438E-01 0.12525E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60112E+03 2 0.24412E-06 0.42188E+02 0.15688E+03 c Velocity[X] 0.14569E+01 c Velocity[Y] 0.10945E+02 c Velocity[Z] 0.29786E+02 c Pressure 0.75832E-01 8 0.95022E-08 0.20510E+07 0.37694E+02 c k 0.24578E+04 1 0.13979E-05 0.84199E+05 0.14692E+04 c omega 0.81515E+09 1 0.44416E-08 0.37993E+12 0.45134E+02 c TotEner 0.24219E+06 1 0.11163E-05 0.47181E+07 0.23648E+02 c temperature 0.00000E+00 0 0.00000E+00 0.87093E+01 0.23807E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9877e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.85 226.85 0.0017791 0.00096277 v Velocity[Y] -0.1301 701.9 250.52 81.011 v Velocity[Z] -19.193 361.76 25.023 1.9637 v ǁVelocityǁ 0.1971 701.9 260.14 83.751 v Pressure 50346 1.1024e+05 1.0356e+05 1.0416e+05 v k 1.1791e-08 42037 910.71 355.41 v omega 154.24 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92482 6.2951e+05 3.416e+05 2.4854e+05 v temperature 64.051 533.95 397.93 337.2 v Density 0.39166 4.7744 0.94911 1.0903 v TurbVisc 8.7805e-19 0.064118 0.010068 0.02864 v CourantNb 1.3143e-05 43.378 0.3908 0.0075947 v FourierNb 4.5076e-05 206.71 1.8389 0.090629 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 64.135 533.95 402.86 421.92 v Boundary Density 0.39177 4.7696 0.98825 0.89833 v Yplus 0 44.821 2.449 0.95637 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8391e-05 44.071 0.48094 0.010621 INSTANT 0.159046165E-01 TIME STEP NUMBER 30143 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.643460394E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560988253E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124022439E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10342E+01 0.58107E+02 Friction velocity uk : 0.10342E+01 0.58107E+02 Dimensionless distance yplus : 0.20557E-01 0.44843E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14438E-01 0.12526E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60112E+03 2 0.24400E-06 0.42277E+02 0.15705E+03 c Velocity[X] 0.14449E+01 c Velocity[Y] 0.10945E+02 c Velocity[Z] 0.29888E+02 c Pressure 0.75836E-01 8 0.93599E-08 0.20638E+07 0.37812E+02 c k 0.24581E+04 1 0.14086E-05 0.84661E+05 0.14731E+04 c omega 0.81515E+09 1 0.42940E-08 0.33425E+12 0.42334E+02 c TotEner 0.24219E+06 1 0.11159E-05 0.47320E+07 0.23683E+02 c temperature 0.00000E+00 0 0.00000E+00 0.87568E+01 0.23872E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9872e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.88 226.88 0.0017802 0.00096597 v Velocity[Y] -0.1301 701.9 250.52 81.011 v Velocity[Z] -19.193 361.89 25.028 1.9638 v ǁVelocityǁ 0.2009 701.9 260.15 83.752 v Pressure 50330 1.1024e+05 1.0355e+05 1.0416e+05 v k 1.1791e-08 42055 910.74 355.41 v omega 154.25 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92421 6.2951e+05 3.416e+05 2.4854e+05 v temperature 63.966 533.95 397.92 337.2 v Density 0.39156 4.7792 0.94911 1.0903 v TurbVisc 8.7802e-19 0.064117 0.010068 0.02864 v CourantNb 1.3145e-05 43.386 0.39086 0.0075949 v FourierNb 4.5077e-05 206.64 1.8387 0.09063 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 64.051 533.95 402.85 421.92 v Boundary Density 0.39166 4.7744 0.98831 0.89834 v Yplus 0 44.843 2.449 0.95644 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8394e-05 44.078 0.48101 0.010621 INSTANT 0.159048795E-01 TIME STEP NUMBER 30144 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.642802340E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560991959E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124047465E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10342E+01 0.58111E+02 Friction velocity uk : 0.10342E+01 0.58111E+02 Dimensionless distance yplus : 0.20557E-01 0.44866E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14438E-01 0.12527E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60112E+03 2 0.24387E-06 0.42361E+02 0.15720E+03 c Velocity[X] 0.14332E+01 c Velocity[Y] 0.10934E+02 c Velocity[Z] 0.29994E+02 c Pressure 0.75840E-01 8 0.91238E-08 0.20769E+07 0.37931E+02 c k 0.24584E+04 1 0.14192E-05 0.85127E+05 0.14770E+04 c omega 0.81515E+09 1 0.38393E-08 0.26036E+12 0.37363E+02 c TotEner 0.24219E+06 1 0.11155E-05 0.47426E+07 0.23709E+02 c temperature 0.00000E+00 0 0.00000E+00 0.88048E+01 0.23937E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9867e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.91 226.91 0.0017812 0.00096916 v Velocity[Y] -0.13009 701.9 250.52 81.012 v Velocity[Z] -19.192 362.01 25.032 1.964 v ǁVelocityǁ 0.20472 701.9 260.15 83.753 v Pressure 50313 1.1024e+05 1.0355e+05 1.0416e+05 v k 1.179e-08 42072 910.78 355.41 v omega 154.25 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92359 6.2951e+05 3.416e+05 2.4854e+05 v temperature 63.881 533.95 397.92 337.2 v Density 0.39145 4.784 0.9491 1.0903 v TurbVisc 8.7799e-19 0.064117 0.010068 0.02864 v CourantNb 1.3147e-05 43.394 0.39093 0.007595 v FourierNb 4.5077e-05 206.58 1.8384 0.090631 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 63.966 533.95 402.85 421.92 v Boundary Density 0.39156 4.7792 0.98837 0.89836 v Yplus 0 44.866 2.4491 0.95651 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8397e-05 44.086 0.48107 0.010621 INSTANT 0.159051425E-01 TIME STEP NUMBER 30145 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.642144104E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560995323E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124071676E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10342E+01 0.58114E+02 Friction velocity uk : 0.10342E+01 0.58114E+02 Dimensionless distance yplus : 0.20556E-01 0.44888E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14438E-01 0.12528E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60113E+03 2 0.24375E-06 0.42452E+02 0.15737E+03 c Velocity[X] 0.14218E+01 c Velocity[Y] 0.10926E+02 c Velocity[Z] 0.30104E+02 c Pressure 0.75844E-01 8 0.89677E-08 0.20904E+07 0.38054E+02 c k 0.24587E+04 1 0.14305E-05 0.85658E+05 0.14815E+04 c omega 0.81515E+09 1 0.37210E-08 0.24644E+12 0.36351E+02 c TotEner 0.24219E+06 1 0.11151E-05 0.47547E+07 0.23739E+02 c temperature 0.00000E+00 0 0.00000E+00 0.88547E+01 0.24005E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9862e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.93 226.93 0.0017819 0.00097234 v Velocity[Y] -0.13009 701.9 250.52 81.013 v Velocity[Z] -19.192 362.13 25.037 1.9642 v ǁVelocityǁ 0.20855 701.9 260.16 83.754 v Pressure 50297 1.1024e+05 1.0355e+05 1.0416e+05 v k 1.179e-08 42089 910.82 355.41 v omega 154.25 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92297 6.2951e+05 3.416e+05 2.4854e+05 v temperature 63.796 533.95 397.92 337.2 v Density 0.39134 4.7889 0.9491 1.0903 v TurbVisc 8.7796e-19 0.064117 0.010068 0.02864 v CourantNb 1.3149e-05 43.402 0.391 0.0075952 v FourierNb 4.5078e-05 206.52 1.8382 0.090632 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 63.881 533.95 402.84 421.92 v Boundary Density 0.39145 4.784 0.98844 0.89837 v Yplus 0 44.888 2.4491 0.95658 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8399e-05 44.093 0.48114 0.010622 INSTANT 0.159054055E-01 TIME STEP NUMBER 30146 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.641486989E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560998374E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124095096E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10341E+01 0.58118E+02 Friction velocity uk : 0.10341E+01 0.58118E+02 Dimensionless distance yplus : 0.20556E-01 0.44911E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14437E-01 0.12529E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60113E+03 2 0.24363E-06 0.42557E+02 0.15756E+03 c Velocity[X] 0.14106E+01 c Velocity[Y] 0.10927E+02 c Velocity[Z] 0.30219E+02 c Pressure 0.75848E-01 8 0.90313E-08 0.21043E+07 0.38181E+02 c k 0.24590E+04 1 0.14424E-05 0.86221E+05 0.14862E+04 c omega 0.81515E+09 1 0.36245E-08 0.24162E+12 0.35993E+02 c TotEner 0.24219E+06 1 0.11148E-05 0.47697E+07 0.23777E+02 c temperature 0.00000E+00 0 0.00000E+00 0.89070E+01 0.24076E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9857e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.96 226.96 0.0017823 0.00097551 v Velocity[Y] -0.13009 701.9 250.52 81.014 v Velocity[Z] -19.191 362.26 25.042 1.9644 v ǁVelocityǁ 0.21238 701.9 260.16 83.755 v Pressure 50281 1.1024e+05 1.0355e+05 1.0416e+05 v k 1.179e-08 42107 910.85 355.41 v omega 154.26 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92235 6.2951e+05 3.416e+05 2.4854e+05 v temperature 63.71 533.95 397.92 337.2 v Density 0.39124 4.7938 0.9491 1.0903 v TurbVisc 8.7793e-19 0.064117 0.010068 0.02864 v CourantNb 1.3151e-05 43.41 0.39107 0.0075953 v FourierNb 4.5079e-05 206.45 1.838 0.090634 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 63.796 533.95 402.84 421.92 v Boundary Density 0.39134 4.7889 0.9885 0.89838 v Yplus 0 44.911 2.4492 0.95665 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8402e-05 44.1 0.48121 0.010622 INSTANT 0.159056685E-01 TIME STEP NUMBER 30147 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.640832294E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561001120E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124117746E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10341E+01 0.58122E+02 Friction velocity uk : 0.10341E+01 0.58122E+02 Dimensionless distance yplus : 0.20556E-01 0.44934E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14437E-01 0.12531E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60113E+03 2 0.24351E-06 0.42667E+02 0.15776E+03 c Velocity[X] 0.13998E+01 c Velocity[Y] 0.10928E+02 c Velocity[Z] 0.30339E+02 c Pressure 0.75852E-01 8 0.93276E-08 0.21186E+07 0.38310E+02 c k 0.24593E+04 1 0.14544E-05 0.86795E+05 0.14910E+04 c omega 0.81515E+09 1 0.40444E-08 0.29620E+12 0.39852E+02 c TotEner 0.24219E+06 1 0.11145E-05 0.47846E+07 0.23814E+02 c temperature 0.00000E+00 0 0.00000E+00 0.89607E+01 0.24148E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9852e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -226.99 226.99 0.0017827 0.00097867 v Velocity[Y] -0.13008 701.9 250.52 81.015 v Velocity[Z] -19.191 362.38 25.047 1.9646 v ǁVelocityǁ 0.21623 701.9 260.16 83.756 v Pressure 50265 1.1024e+05 1.0355e+05 1.0416e+05 v k 1.1789e-08 42124 910.89 355.41 v omega 154.26 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92172 6.2951e+05 3.416e+05 2.4854e+05 v temperature 63.624 533.95 397.92 337.2 v Density 0.39113 4.7987 0.94909 1.0903 v TurbVisc 8.7791e-19 0.064117 0.010068 0.028641 v CourantNb 1.3152e-05 43.419 0.39113 0.0075954 v FourierNb 4.508e-05 206.39 1.8377 0.090635 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 63.71 533.95 402.83 421.91 v Boundary Density 0.39124 4.7938 0.98856 0.8984 v Yplus 0 44.934 2.4492 0.95672 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8404e-05 44.107 0.48128 0.010622 INSTANT 0.159059315E-01 TIME STEP NUMBER 30148 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.640181314E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561003560E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124139648E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10341E+01 0.58125E+02 Friction velocity uk : 0.10341E+01 0.58125E+02 Dimensionless distance yplus : 0.20556E-01 0.44957E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14437E-01 0.12532E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60113E+03 2 0.24338E-06 0.42783E+02 0.15798E+03 c Velocity[X] 0.13892E+01 c Velocity[Y] 0.10930E+02 c Velocity[Z] 0.30464E+02 c Pressure 0.75856E-01 8 0.91345E-08 0.21332E+07 0.38442E+02 c k 0.24596E+04 1 0.14667E-05 0.87371E+05 0.14958E+04 c omega 0.81515E+09 1 0.45235E-08 0.31956E+12 0.41393E+02 c TotEner 0.24220E+06 1 0.11142E-05 0.47997E+07 0.23851E+02 c temperature 0.00000E+00 0 0.00000E+00 0.90156E+01 0.24222E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9848e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.01 227.01 0.001783 0.00098183 v Velocity[Y] -0.13008 701.9 250.53 81.016 v Velocity[Z] -19.19 362.5 25.052 1.9648 v ǁVelocityǁ 0.22009 701.9 260.17 83.756 v Pressure 50249 1.1024e+05 1.0355e+05 1.0416e+05 v k 1.1789e-08 42142 910.93 355.41 v omega 154.27 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92109 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 63.537 533.95 397.92 337.2 v Density 0.39103 4.8037 0.94909 1.0903 v TurbVisc 8.7788e-19 0.064117 0.010069 0.028641 v CourantNb 1.3154e-05 43.427 0.3912 0.0075956 v FourierNb 4.508e-05 206.33 1.8375 0.090636 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 63.624 533.95 402.83 421.91 v Boundary Density 0.39113 4.7987 0.98863 0.89841 v Yplus 0 44.957 2.4492 0.95679 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8406e-05 44.114 0.48135 0.010622 INSTANT 0.159061945E-01 TIME STEP NUMBER 30149 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.639535339E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561005705E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124160822E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10341E+01 0.58129E+02 Friction velocity uk : 0.10341E+01 0.58129E+02 Dimensionless distance yplus : 0.20556E-01 0.44980E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14437E-01 0.12533E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60113E+03 2 0.24326E-06 0.42894E+02 0.15818E+03 c Velocity[X] 0.13789E+01 c Velocity[Y] 0.10922E+02 c Velocity[Z] 0.30593E+02 c Pressure 0.75860E-01 8 0.89956E-08 0.21484E+07 0.38579E+02 c k 0.24599E+04 1 0.14789E-05 0.87969E+05 0.15008E+04 c omega 0.81515E+09 1 0.53788E-08 0.48342E+12 0.50911E+02 c TotEner 0.24220E+06 1 0.11138E-05 0.48133E+07 0.23885E+02 c temperature 0.00000E+00 0 0.00000E+00 0.90717E+01 0.24297E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9843e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.04 227.04 0.0017832 0.00098499 v Velocity[Y] -0.13008 701.9 250.53 81.017 v Velocity[Z] -19.19 362.63 25.057 1.965 v ǁVelocityǁ 0.22395 701.9 260.17 83.757 v Pressure 50233 1.1024e+05 1.0355e+05 1.0416e+05 v k 1.1789e-08 42159 910.97 355.41 v omega 154.27 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 92046 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 63.45 533.95 397.92 337.2 v Density 0.39092 4.8087 0.94908 1.0903 v TurbVisc 8.7785e-19 0.064117 0.010069 0.028641 v CourantNb 1.3156e-05 43.435 0.39127 0.0075957 v FourierNb 4.5081e-05 206.27 1.8373 0.090637 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 63.537 533.95 402.82 421.91 v Boundary Density 0.39103 4.8037 0.98869 0.89842 v Yplus 0 44.98 2.4493 0.95686 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8409e-05 44.121 0.48142 0.010622 INSTANT 0.159064576E-01 TIME STEP NUMBER 30150 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.638895649E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561007563E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124181287E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10341E+01 0.58133E+02 Friction velocity uk : 0.10341E+01 0.58133E+02 Dimensionless distance yplus : 0.20555E-01 0.45003E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14437E-01 0.12534E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60114E+03 2 0.24314E-06 0.43014E+02 0.15840E+03 c Velocity[X] 0.13688E+01 c Velocity[Y] 0.10918E+02 c Velocity[Z] 0.30727E+02 c Pressure 0.75864E-01 8 0.88402E-08 0.21639E+07 0.38717E+02 c k 0.24602E+04 1 0.14911E-05 0.88576E+05 0.15059E+04 c omega 0.81515E+09 1 0.49434E-08 0.38062E+12 0.45175E+02 c TotEner 0.24220E+06 1 0.11135E-05 0.48284E+07 0.23922E+02 c temperature 0.00000E+00 0 0.00000E+00 0.91294E+01 0.24374E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9838e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.07 227.07 0.0017834 0.00098814 v Velocity[Y] -0.13007 701.9 250.53 81.018 v Velocity[Z] -19.189 362.75 25.062 1.9652 v ǁVelocityǁ 0.22411 701.9 260.17 83.758 v Pressure 50217 1.1024e+05 1.0355e+05 1.0416e+05 v k 1.1788e-08 42177 911 355.41 v omega 154.28 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 91982 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 63.363 533.95 397.92 337.2 v Density 0.39082 4.8138 0.94908 1.0903 v TurbVisc 8.7782e-19 0.064117 0.010069 0.028641 v CourantNb 1.3157e-05 43.443 0.39133 0.0075958 v FourierNb 4.5082e-05 206.21 1.837 0.090639 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 63.45 533.95 402.81 421.91 v Boundary Density 0.39092 4.8087 0.98876 0.89844 v Yplus 0 45.003 2.4494 0.95694 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8411e-05 44.128 0.48149 0.010623 INSTANT 0.159067206E-01 TIME STEP NUMBER 30151 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.638263517E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561009140E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124201060E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10341E+01 0.58136E+02 Friction velocity uk : 0.10341E+01 0.58136E+02 Dimensionless distance yplus : 0.20555E-01 0.45027E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14437E-01 0.12536E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60114E+03 2 0.24302E-06 0.43155E+02 0.15866E+03 c Velocity[X] 0.13590E+01 c Velocity[Y] 0.10929E+02 c Velocity[Z] 0.30866E+02 c Pressure 0.75868E-01 8 0.89317E-08 0.21798E+07 0.38860E+02 c k 0.24605E+04 1 0.15047E-05 0.89288E+05 0.15118E+04 c omega 0.81515E+09 1 0.46383E-08 0.36345E+12 0.44144E+02 c TotEner 0.24220E+06 1 0.11133E-05 0.48479E+07 0.23970E+02 c temperature 0.00000E+00 0 0.00000E+00 0.91900E+01 0.24455E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9833e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.1 227.1 0.0017834 0.00099128 v Velocity[Y] -0.13007 701.9 250.53 81.019 v Velocity[Z] -19.189 362.87 25.066 1.9654 v ǁVelocityǁ 0.2242 701.9 260.18 83.759 v Pressure 50201 1.1024e+05 1.0355e+05 1.0416e+05 v k 1.1788e-08 42195 911.04 355.41 v omega 154.28 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 91918 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 63.275 533.95 397.91 337.2 v Density 0.39071 4.8188 0.94908 1.0903 v TurbVisc 8.7779e-19 0.064116 0.010069 0.028641 v CourantNb 1.3159e-05 43.451 0.3914 0.007596 v FourierNb 4.5083e-05 206.15 1.8368 0.09064 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 63.363 533.95 402.81 421.91 v Boundary Density 0.39082 4.8138 0.98882 0.89845 v Yplus 0 45.027 2.4494 0.95701 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8413e-05 44.135 0.48155 0.010623 INSTANT 0.159069836E-01 TIME STEP NUMBER 30152 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.637640207E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561010447E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124220158E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10341E+01 0.58140E+02 Friction velocity uk : 0.10341E+01 0.58140E+02 Dimensionless distance yplus : 0.20555E-01 0.45050E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14437E-01 0.12537E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60114E+03 2 0.24290E-06 0.43320E+02 0.15896E+03 c Velocity[X] 0.13495E+01 c Velocity[Y] 0.10959E+02 c Velocity[Z] 0.31011E+02 c Pressure 0.75872E-01 8 0.91951E-08 0.21964E+07 0.39007E+02 c k 0.24608E+04 1 0.15194E-05 0.90077E+05 0.15183E+04 c omega 0.81515E+09 1 0.48192E-08 0.39705E+12 0.46140E+02 c TotEner 0.24220E+06 1 0.11130E-05 0.48726E+07 0.24032E+02 c temperature 0.00000E+00 0 0.00000E+00 0.92540E+01 0.24540E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9829e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.12 227.12 0.0017836 0.00099442 v Velocity[Y] -0.13007 701.9 250.53 81.02 v Velocity[Z] -19.188 363 25.071 1.9655 v ǁVelocityǁ 0.22428 701.9 260.18 83.76 v Pressure 50185 1.1024e+05 1.0354e+05 1.0416e+05 v k 1.1787e-08 42213 911.08 355.4 v omega 154.29 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 91854 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 63.186 533.95 397.91 337.2 v Density 0.39061 4.824 0.94907 1.0903 v TurbVisc 8.7776e-19 0.064116 0.010069 0.028641 v CourantNb 1.316e-05 43.459 0.39147 0.0075961 v FourierNb 4.5084e-05 206.09 1.8365 0.090641 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 63.275 533.95 402.8 421.91 v Boundary Density 0.39071 4.8188 0.98889 0.89846 v Yplus 0 45.05 2.4495 0.95708 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8416e-05 44.142 0.48162 0.010623 INSTANT 0.159072466E-01 TIME STEP NUMBER 30153 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.637026969E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561011493E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124238597E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10341E+01 0.58144E+02 Friction velocity uk : 0.10341E+01 0.58144E+02 Dimensionless distance yplus : 0.20555E-01 0.45074E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14436E-01 0.12538E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60114E+03 2 0.24279E-06 0.43502E+02 0.15929E+03 c Velocity[X] 0.13403E+01 c Velocity[Y] 0.11001E+02 c Velocity[Z] 0.31161E+02 c Pressure 0.75876E-01 8 0.95987E-08 0.22133E+07 0.39157E+02 c k 0.24612E+04 1 0.15340E-05 0.90828E+05 0.15245E+04 c omega 0.81515E+09 1 0.47608E-08 0.45557E+12 0.49423E+02 c TotEner 0.24220E+06 1 0.11129E-05 0.48996E+07 0.24098E+02 c temperature 0.00000E+00 0 0.00000E+00 0.93200E+01 0.24627E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9824e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.15 227.15 0.0017837 0.00099756 v Velocity[Y] -0.13006 701.9 250.53 81.021 v Velocity[Z] -19.188 363.12 25.076 1.9657 v ǁVelocityǁ 0.22437 701.9 260.18 83.761 v Pressure 50169 1.1024e+05 1.0354e+05 1.0416e+05 v k 1.1787e-08 42230 911.11 355.4 v omega 154.29 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 91790 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 63.097 533.95 397.91 337.2 v Density 0.3905 4.8291 0.94907 1.0903 v TurbVisc 8.7773e-19 0.064116 0.010069 0.028642 v CourantNb 1.3162e-05 43.467 0.39153 0.0075963 v FourierNb 4.5085e-05 206.03 1.8363 0.090642 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 63.186 533.95 402.8 421.91 v Boundary Density 0.39061 4.824 0.98895 0.89848 v Yplus 0 45.074 2.4495 0.95716 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8418e-05 44.149 0.48169 0.010623 INSTANT 0.159075096E-01 TIME STEP NUMBER 30154 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.636425042E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561012292E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124256390E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10341E+01 0.58147E+02 Friction velocity uk : 0.10341E+01 0.58147E+02 Dimensionless distance yplus : 0.20555E-01 0.45098E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14436E-01 0.12539E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60114E+03 2 0.24267E-06 0.43622E+02 0.15951E+03 c Velocity[X] 0.13312E+01 c Velocity[Y] 0.10975E+02 c Velocity[Z] 0.31316E+02 c Pressure 0.75880E-01 8 0.99750E-08 0.22308E+07 0.39311E+02 c k 0.24615E+04 1 0.15471E-05 0.91441E+05 0.15295E+04 c omega 0.81515E+09 1 0.48120E-08 0.41409E+12 0.47119E+02 c TotEner 0.24220E+06 1 0.11126E-05 0.49087E+07 0.24120E+02 c temperature 0.00000E+00 0 0.00000E+00 0.93816E+01 0.24708E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9819e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.18 227.18 0.0017839 0.0010007 v Velocity[Y] -0.13006 701.9 250.53 81.022 v Velocity[Z] -19.187 363.24 25.081 1.9659 v ǁVelocityǁ 0.22445 701.9 260.19 83.762 v Pressure 50153 1.1024e+05 1.0354e+05 1.0416e+05 v k 1.1787e-08 42248 911.15 355.4 v omega 154.3 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 91725 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 63.008 533.95 397.91 337.2 v Density 0.3904 4.8343 0.94906 1.0903 v TurbVisc 8.777e-19 0.064116 0.010069 0.028642 v CourantNb 1.3164e-05 43.475 0.3916 0.0075964 v FourierNb 4.5086e-05 205.98 1.8361 0.090643 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 63.097 533.95 402.79 421.91 v Boundary Density 0.3905 4.8291 0.98902 0.89849 v Yplus 0 45.098 2.4496 0.95723 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.842e-05 44.156 0.48176 0.010623 INSTANT 0.159077726E-01 TIME STEP NUMBER 30155 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.635835652E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561012853E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124273551E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10341E+01 0.58151E+02 Friction velocity uk : 0.10341E+01 0.58151E+02 Dimensionless distance yplus : 0.20555E-01 0.45122E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14436E-01 0.12541E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60114E+03 2 0.24255E-06 0.43737E+02 0.15972E+03 c Velocity[X] 0.13223E+01 c Velocity[Y] 0.10940E+02 c Velocity[Z] 0.31475E+02 c Pressure 0.75884E-01 8 0.96436E-08 0.22483E+07 0.39466E+02 c k 0.24618E+04 1 0.15598E-05 0.92070E+05 0.15346E+04 c omega 0.81516E+09 1 0.46498E-08 0.40941E+12 0.46852E+02 c TotEner 0.24221E+06 1 0.11123E-05 0.49167E+07 0.24140E+02 c temperature 0.00000E+00 0 0.00000E+00 0.94443E+01 0.24791E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9815e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.2 227.2 0.0017842 0.0010038 v Velocity[Y] -0.13006 701.9 250.53 81.023 v Velocity[Z] -19.187 363.36 25.086 1.9661 v ǁVelocityǁ 0.22453 701.9 260.19 83.763 v Pressure 50137 1.1024e+05 1.0354e+05 1.0416e+05 v k 1.1786e-08 42266 911.19 355.4 v omega 154.3 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 91659 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 62.918 533.95 397.91 337.2 v Density 0.39029 4.8396 0.94906 1.0903 v TurbVisc 8.7768e-19 0.064116 0.010069 0.028642 v CourantNb 1.3165e-05 43.483 0.39167 0.0075965 v FourierNb 4.5087e-05 205.92 1.8359 0.090645 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 63.008 533.95 402.79 421.91 v Boundary Density 0.3904 4.8343 0.98909 0.89851 v Yplus 0 45.122 2.4496 0.95731 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8422e-05 44.163 0.48183 0.010623 INSTANT 0.159080357E-01 TIME STEP NUMBER 30156 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.635260007E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561013175E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124290092E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10341E+01 0.58155E+02 Friction velocity uk : 0.10341E+01 0.58155E+02 Dimensionless distance yplus : 0.20554E-01 0.45146E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14436E-01 0.12542E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60115E+03 2 0.24243E-06 0.43881E+02 0.15998E+03 c Velocity[X] 0.13137E+01 c Velocity[Y] 0.10927E+02 c Velocity[Z] 0.31641E+02 c Pressure 0.75888E-01 8 0.98298E-08 0.22665E+07 0.39625E+02 c k 0.24621E+04 1 0.15734E-05 0.92782E+05 0.15404E+04 c omega 0.81516E+09 1 0.41860E-08 0.37583E+12 0.44889E+02 c TotEner 0.24221E+06 1 0.11120E-05 0.49317E+07 0.24177E+02 c temperature 0.00000E+00 0 0.00000E+00 0.95110E+01 0.24878E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.981e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.23 227.23 0.0017845 0.001007 v Velocity[Y] -0.13005 701.9 250.53 81.024 v Velocity[Z] -19.186 363.49 25.091 1.9663 v ǁVelocityǁ 0.22462 701.9 260.2 83.764 v Pressure 50121 1.1024e+05 1.0354e+05 1.0416e+05 v k 1.1786e-08 42284 911.22 355.4 v omega 154.31 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 91594 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 62.828 533.95 397.91 337.2 v Density 0.39019 4.8448 0.94906 1.0903 v TurbVisc 8.7765e-19 0.064116 0.01007 0.028642 v CourantNb 1.3166e-05 43.491 0.39173 0.0075967 v FourierNb 4.5088e-05 205.86 1.8356 0.090646 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 62.918 533.95 402.78 421.9 v Boundary Density 0.39029 4.8396 0.98916 0.89852 v Yplus 0 45.146 2.4497 0.95738 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8424e-05 44.17 0.48189 0.010624 INSTANT 0.159082987E-01 TIME STEP NUMBER 30157 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.634699300E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561013260E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124306023E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10340E+01 0.58158E+02 Friction velocity uk : 0.10340E+01 0.58158E+02 Dimensionless distance yplus : 0.20554E-01 0.45171E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14436E-01 0.12543E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60115E+03 2 0.24232E-06 0.44047E+02 0.16028E+03 c Velocity[X] 0.13053E+01 c Velocity[Y] 0.10929E+02 c Velocity[Z] 0.31812E+02 c Pressure 0.75892E-01 9 0.88283E-08 0.22851E+07 0.39787E+02 c k 0.24624E+04 1 0.15877E-05 0.93550E+05 0.15467E+04 c omega 0.81516E+09 1 0.42110E-08 0.39941E+12 0.46276E+02 c TotEner 0.24221E+06 1 0.11118E-05 0.49507E+07 0.24223E+02 c temperature 0.00000E+00 0 0.00000E+00 0.95803E+01 0.24969E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9805e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.26 227.26 0.0017847 0.0010101 v Velocity[Y] -0.13005 701.9 250.53 81.025 v Velocity[Z] -19.186 363.61 25.096 1.9665 v ǁVelocityǁ 0.2247 701.9 260.2 83.765 v Pressure 50105 1.1024e+05 1.0354e+05 1.0416e+05 v k 1.1786e-08 42302 911.26 355.4 v omega 154.31 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 91528 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 62.737 533.95 397.91 337.2 v Density 0.39008 4.8502 0.94905 1.0903 v TurbVisc 8.7762e-19 0.064116 0.01007 0.028642 v CourantNb 1.3168e-05 43.499 0.3918 0.0075968 v FourierNb 4.5089e-05 205.81 1.8354 0.090647 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 62.828 533.95 402.77 421.9 v Boundary Density 0.39019 4.8448 0.98922 0.89853 v Yplus 0 45.171 2.4497 0.95746 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8426e-05 44.177 0.48196 0.010624 INSTANT 0.159085617E-01 TIME STEP NUMBER 30158 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.634154705E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561013104E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124321354E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10340E+01 0.58162E+02 Friction velocity uk : 0.10340E+01 0.58162E+02 Dimensionless distance yplus : 0.20554E-01 0.45195E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14436E-01 0.12544E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60115E+03 2 0.24220E-06 0.44212E+02 0.16058E+03 c Velocity[X] 0.12971E+01 c Velocity[Y] 0.10925E+02 c Velocity[Z] 0.31989E+02 c Pressure 0.75896E-01 8 0.97956E-08 0.23044E+07 0.39956E+02 c k 0.24628E+04 1 0.16023E-05 0.94338E+05 0.15530E+04 c omega 0.81516E+09 1 0.44587E-08 0.37889E+12 0.45072E+02 c TotEner 0.24221E+06 1 0.11116E-05 0.49691E+07 0.24268E+02 c temperature 0.00000E+00 0 0.00000E+00 0.96512E+01 0.25061E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9801e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.28 227.28 0.0017848 0.0010132 v Velocity[Y] -0.13005 701.9 250.53 81.026 v Velocity[Z] -19.185 363.73 25.1 1.9667 v ǁVelocityǁ 0.22478 701.9 260.2 83.766 v Pressure 50089 1.1024e+05 1.0354e+05 1.0416e+05 v k 1.1785e-08 42320 911.3 355.4 v omega 154.32 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 91461 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 62.646 533.95 397.9 337.2 v Density 0.38998 4.8555 0.94905 1.0903 v TurbVisc 8.7759e-19 0.064116 0.01007 0.028642 v CourantNb 1.3169e-05 43.507 0.39186 0.007597 v FourierNb 4.509e-05 205.75 1.8352 0.090648 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 62.737 533.95 402.77 421.9 v Boundary Density 0.39008 4.8502 0.98929 0.89855 v Yplus 0 45.195 2.4498 0.95754 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8428e-05 44.184 0.48203 0.010624 INSTANT 0.159088247E-01 TIME STEP NUMBER 30159 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.633627378E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561012709E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124336094E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10340E+01 0.58166E+02 Friction velocity uk : 0.10340E+01 0.58166E+02 Dimensionless distance yplus : 0.20554E-01 0.45220E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14436E-01 0.12546E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60115E+03 2 0.24209E-06 0.44387E+02 0.16090E+03 c Velocity[X] 0.12892E+01 c Velocity[Y] 0.10925E+02 c Velocity[Z] 0.32172E+02 c Pressure 0.75900E-01 8 0.95260E-08 0.23242E+07 0.40126E+02 c k 0.24631E+04 1 0.16170E-05 0.95148E+05 0.15595E+04 c omega 0.81516E+09 1 0.45276E-08 0.49133E+12 0.51326E+02 c TotEner 0.24221E+06 1 0.11114E-05 0.49888E+07 0.24316E+02 c temperature 0.00000E+00 0 0.00000E+00 0.97239E+01 0.25155E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9796e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.31 227.31 0.0017849 0.0010163 v Velocity[Y] -0.13004 701.9 250.53 81.027 v Velocity[Z] -19.185 363.86 25.105 1.9669 v ǁVelocityǁ 0.22486 701.9 260.21 83.767 v Pressure 50073 1.1024e+05 1.0354e+05 1.0416e+05 v k 1.1785e-08 42338 911.34 355.4 v omega 154.32 9.6784e+09 1.8459e+08 3.4144e+05 v TotEner 91394 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 62.554 533.95 397.9 337.2 v Density 0.38987 4.8609 0.94904 1.0903 v TurbVisc 8.7757e-19 0.064115 0.01007 0.028643 v CourantNb 1.317e-05 43.515 0.39193 0.0075971 v FourierNb 4.5091e-05 205.7 1.835 0.090649 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 62.646 533.95 402.76 421.9 v Boundary Density 0.38998 4.8555 0.98936 0.89856 v Yplus 0 45.22 2.4499 0.95761 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.843e-05 44.19 0.4821 0.010624 INSTANT 0.159090877E-01 TIME STEP NUMBER 30160 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.633118458E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561012073E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124350252E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10340E+01 0.58169E+02 Friction velocity uk : 0.10340E+01 0.58169E+02 Dimensionless distance yplus : 0.20554E-01 0.45245E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14436E-01 0.12547E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60115E+03 2 0.24197E-06 0.44575E+02 0.16124E+03 c Velocity[X] 0.12814E+01 c Velocity[Y] 0.10932E+02 c Velocity[Z] 0.32361E+02 c Pressure 0.75904E-01 8 0.94906E-08 0.23445E+07 0.40302E+02 c k 0.24634E+04 1 0.16319E-05 0.95987E+05 0.15663E+04 c omega 0.81516E+09 1 0.41336E-08 0.40539E+12 0.46621E+02 c TotEner 0.24221E+06 1 0.11112E-05 0.50109E+07 0.24370E+02 c temperature 0.00000E+00 0 0.00000E+00 0.97992E+01 0.25252E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9791e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.34 227.34 0.0017849 0.0010194 v Velocity[Y] -0.13004 701.9 250.53 81.028 v Velocity[Z] -19.184 363.98 25.11 1.9671 v ǁVelocityǁ 0.22494 701.9 260.21 83.768 v Pressure 50057 1.1024e+05 1.0354e+05 1.0416e+05 v k 1.1785e-08 42357 911.38 355.4 v omega 154.33 9.6784e+09 1.846e+08 3.4144e+05 v TotEner 91327 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 62.462 533.95 397.9 337.2 v Density 0.38977 4.8664 0.94904 1.0903 v TurbVisc 8.7754e-19 0.064115 0.01007 0.028643 v CourantNb 1.3172e-05 43.523 0.392 0.0075972 v FourierNb 4.5092e-05 205.64 1.8347 0.090651 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 62.554 533.95 402.76 421.9 v Boundary Density 0.38987 4.8609 0.98943 0.89858 v Yplus 0 45.245 2.4499 0.95769 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8431e-05 44.197 0.48216 0.010624 INSTANT 0.159093508E-01 TIME STEP NUMBER 30161 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.632629058E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561011195E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124363832E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10340E+01 0.58173E+02 Friction velocity uk : 0.10340E+01 0.58173E+02 Dimensionless distance yplus : 0.20553E-01 0.45270E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14435E-01 0.12548E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60115E+03 2 0.24186E-06 0.44756E+02 0.16156E+03 c Velocity[X] 0.12739E+01 c Velocity[Y] 0.10925E+02 c Velocity[Z] 0.32556E+02 c Pressure 0.75908E-01 8 0.97542E-08 0.23653E+07 0.40480E+02 c k 0.24638E+04 1 0.16475E-05 0.96874E+05 0.15733E+04 c omega 0.81516E+09 1 0.40362E-08 0.33499E+12 0.42381E+02 c TotEner 0.24222E+06 1 0.11111E-05 0.50298E+07 0.24416E+02 c temperature 0.00000E+00 0 0.00000E+00 0.98746E+01 0.25349E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9787e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.36 227.36 0.0017851 0.0010225 v Velocity[Y] -0.13004 701.9 250.53 81.028 v Velocity[Z] -19.184 364.1 25.115 1.9673 v ǁVelocityǁ 0.22502 701.9 260.21 83.768 v Pressure 50041 1.1024e+05 1.0354e+05 1.0416e+05 v k 1.1784e-08 42375 911.42 355.4 v omega 154.33 9.6785e+09 1.846e+08 3.4144e+05 v TotEner 91260 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 62.369 533.95 397.9 337.2 v Density 0.38966 4.8719 0.94903 1.0903 v TurbVisc 8.7751e-19 0.064115 0.01007 0.028643 v CourantNb 1.3173e-05 43.531 0.39206 0.0075974 v FourierNb 4.5093e-05 205.59 1.8345 0.090652 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 62.462 533.95 402.75 421.9 v Boundary Density 0.38977 4.8664 0.9895 0.89859 v Yplus 0 45.27 2.45 0.95777 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8433e-05 44.204 0.48223 0.010625 INSTANT 0.159096138E-01 TIME STEP NUMBER 30162 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.632160269E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561010063E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124376843E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10340E+01 0.58177E+02 Friction velocity uk : 0.10340E+01 0.58177E+02 Dimensionless distance yplus : 0.20553E-01 0.45295E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14435E-01 0.12550E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60116E+03 2 0.24174E-06 0.44946E+02 0.16190E+03 c Velocity[X] 0.12666E+01 c Velocity[Y] 0.10921E+02 c Velocity[Z] 0.32758E+02 c Pressure 0.75912E-01 8 0.95443E-08 0.23866E+07 0.40662E+02 c k 0.24641E+04 1 0.16630E-05 0.97745E+05 0.15803E+04 c omega 0.81516E+09 1 0.54964E-08 0.45481E+12 0.49382E+02 c TotEner 0.24222E+06 1 0.11109E-05 0.50502E+07 0.24465E+02 c temperature 0.00000E+00 0 0.00000E+00 0.99521E+01 0.25448E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9782e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.39 227.39 0.0017853 0.0010256 v Velocity[Y] -0.13004 701.9 250.53 81.029 v Velocity[Z] -19.183 364.22 25.12 1.9675 v ǁVelocityǁ 0.2251 701.9 260.22 83.769 v Pressure 50025 1.1024e+05 1.0353e+05 1.0416e+05 v k 1.1784e-08 42393 911.45 355.4 v omega 154.34 9.6785e+09 1.846e+08 3.4144e+05 v TotEner 91192 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 62.276 533.95 397.9 337.2 v Density 0.38956 4.8775 0.94903 1.0903 v TurbVisc 8.7748e-19 0.064115 0.01007 0.028643 v CourantNb 1.3174e-05 43.539 0.39213 0.0075975 v FourierNb 4.5095e-05 205.53 1.8343 0.090653 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 62.369 533.95 402.74 421.9 v Boundary Density 0.38966 4.8719 0.98957 0.89861 v Yplus 0 45.295 2.4501 0.95785 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8435e-05 44.211 0.4823 0.010625 INSTANT 0.159098768E-01 TIME STEP NUMBER 30163 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.631713161E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561008668E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124389289E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10340E+01 0.58180E+02 Friction velocity uk : 0.10340E+01 0.58180E+02 Dimensionless distance yplus : 0.20553E-01 0.45321E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14435E-01 0.12551E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60116E+03 2 0.24163E-06 0.45151E+02 0.16227E+03 c Velocity[X] 0.12595E+01 c Velocity[Y] 0.10926E+02 c Velocity[Z] 0.32965E+02 c Pressure 0.75916E-01 8 0.95619E-08 0.24084E+07 0.40847E+02 c k 0.24644E+04 1 0.16793E-05 0.98687E+05 0.15877E+04 c omega 0.81516E+09 1 0.48700E-08 0.38325E+12 0.45330E+02 c TotEner 0.24222E+06 1 0.11108E-05 0.50731E+07 0.24520E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10032E+02 0.25550E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9777e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.41 227.41 0.0017855 0.0010286 v Velocity[Y] -0.13003 701.9 250.53 81.03 v Velocity[Z] -19.183 364.35 25.125 1.9677 v ǁVelocityǁ 0.22518 701.9 260.22 83.77 v Pressure 50009 1.1024e+05 1.0353e+05 1.0416e+05 v k 1.1783e-08 42412 911.49 355.39 v omega 154.34 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 91123 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 62.182 533.95 397.9 337.2 v Density 0.38946 4.883 0.94903 1.0902 v TurbVisc 8.7745e-19 0.064115 0.01007 0.028643 v CourantNb 1.3175e-05 43.547 0.39219 0.0075976 v FourierNb 4.5096e-05 205.48 1.8341 0.090654 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 62.276 533.95 402.74 421.9 v Boundary Density 0.38956 4.8775 0.98964 0.89862 v Yplus 0 45.321 2.4501 0.95793 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8436e-05 44.218 0.48236 0.010625 INSTANT 0.159101398E-01 TIME STEP NUMBER 30164 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.631288776E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561007010E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124401174E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10340E+01 0.58184E+02 Friction velocity uk : 0.10340E+01 0.58184E+02 Dimensionless distance yplus : 0.20553E-01 0.45347E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14435E-01 0.12552E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60116E+03 2 0.24152E-06 0.45357E+02 0.16264E+03 c Velocity[X] 0.12526E+01 c Velocity[Y] 0.10925E+02 c Velocity[Z] 0.33180E+02 c Pressure 0.75920E-01 8 0.95949E-08 0.24309E+07 0.41037E+02 c k 0.24648E+04 1 0.16961E-05 0.99661E+05 0.15954E+04 c omega 0.81516E+09 1 0.46247E-08 0.33437E+12 0.42341E+02 c TotEner 0.24222E+06 1 0.11107E-05 0.50955E+07 0.24574E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10114E+02 0.25654E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9773e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.44 227.44 0.0017856 0.0010317 v Velocity[Y] -0.13003 701.9 250.53 81.031 v Velocity[Z] -19.182 364.47 25.13 1.9678 v ǁVelocityǁ 0.22526 701.9 260.23 83.771 v Pressure 49993 1.1024e+05 1.0353e+05 1.0416e+05 v k 1.1783e-08 42430 911.53 355.39 v omega 154.35 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 91055 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 62.088 533.95 397.9 337.2 v Density 0.38935 4.8887 0.94902 1.0902 v TurbVisc 8.7743e-19 0.064115 0.01007 0.028643 v CourantNb 1.3176e-05 43.555 0.39226 0.0075978 v FourierNb 4.5097e-05 205.43 1.8339 0.090655 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 62.182 533.95 402.73 421.9 v Boundary Density 0.38946 4.883 0.98972 0.89864 v Yplus 0 45.347 2.4502 0.95801 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8438e-05 44.225 0.48243 0.010625 INSTANT 0.159104028E-01 TIME STEP NUMBER 30165 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.630888133E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561005096E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124412502E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10340E+01 0.58187E+02 Friction velocity uk : 0.10340E+01 0.58187E+02 Dimensionless distance yplus : 0.20553E-01 0.45373E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14435E-01 0.12554E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60116E+03 2 0.24141E-06 0.45599E+02 0.16307E+03 c Velocity[X] 0.12460E+01 c Velocity[Y] 0.10953E+02 c Velocity[Z] 0.33401E+02 c Pressure 0.75924E-01 8 0.94933E-08 0.24539E+07 0.41231E+02 c k 0.24651E+04 1 0.17144E-05 0.10075E+06 0.16039E+04 c omega 0.81516E+09 1 0.41709E-08 0.31666E+12 0.41204E+02 c TotEner 0.24222E+06 1 0.11107E-05 0.51266E+07 0.24649E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10199E+02 0.25762E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9768e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.47 227.47 0.0017858 0.0010348 v Velocity[Y] -0.13003 701.9 250.53 81.032 v Velocity[Z] -19.182 364.59 25.135 1.968 v ǁVelocityǁ 0.22534 701.9 260.23 83.772 v Pressure 49977 1.1024e+05 1.0353e+05 1.0416e+05 v k 1.1783e-08 42449 911.58 355.39 v omega 154.35 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 90985 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 61.993 533.95 397.89 337.2 v Density 0.38925 4.8944 0.94902 1.0902 v TurbVisc 8.774e-19 0.064115 0.01007 0.028644 v CourantNb 1.3177e-05 43.563 0.39233 0.0075979 v FourierNb 4.5098e-05 205.37 1.8337 0.090656 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 62.088 533.95 402.72 421.89 v Boundary Density 0.38935 4.8887 0.98979 0.89865 v Yplus 0 45.373 2.4503 0.95809 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8439e-05 44.232 0.4825 0.010625 INSTANT 0.159106659E-01 TIME STEP NUMBER 30166 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.630512223E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561002933E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124423276E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10340E+01 0.58191E+02 Friction velocity uk : 0.10340E+01 0.58191E+02 Dimensionless distance yplus : 0.20553E-01 0.45399E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14435E-01 0.12555E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60116E+03 2 0.24130E-06 0.45797E+02 0.16342E+03 c Velocity[X] 0.12395E+01 c Velocity[Y] 0.10929E+02 c Velocity[Z] 0.33628E+02 c Pressure 0.75928E-01 8 0.91199E-08 0.24774E+07 0.41428E+02 c k 0.24655E+04 1 0.17295E-05 0.10166E+06 0.16110E+04 c omega 0.81516E+09 1 0.42926E-08 0.36288E+12 0.44109E+02 c TotEner 0.24222E+06 1 0.11106E-05 0.51423E+07 0.24687E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10282E+02 0.25866E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9764e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.49 227.49 0.0017861 0.0010378 v Velocity[Y] -0.13002 701.9 250.54 81.033 v Velocity[Z] -19.181 364.71 25.139 1.9682 v ǁVelocityǁ 0.22541 701.9 260.23 83.773 v Pressure 49961 1.1024e+05 1.0353e+05 1.0416e+05 v k 1.1782e-08 42467 911.62 355.39 v omega 154.36 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 90916 6.2951e+05 3.4161e+05 2.4854e+05 v temperature 61.897 533.95 397.89 337.2 v Density 0.38914 4.9001 0.94901 1.0902 v TurbVisc 8.7737e-19 0.064115 0.010071 0.028644 v CourantNb 1.3178e-05 43.571 0.39239 0.0075981 v FourierNb 4.51e-05 205.32 1.8334 0.090658 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 61.993 533.95 402.72 421.89 v Boundary Density 0.38925 4.8944 0.98986 0.89867 v Yplus 0 45.399 2.4503 0.95817 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.844e-05 44.238 0.48257 0.010626 INSTANT 0.159109289E-01 TIME STEP NUMBER 30167 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.630162008E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.561000532E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124433499E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10340E+01 0.58195E+02 Friction velocity uk : 0.10340E+01 0.58195E+02 Dimensionless distance yplus : 0.20552E-01 0.45425E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14435E-01 0.12557E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60117E+03 2 0.24119E-06 0.46025E+02 0.16383E+03 c Velocity[X] 0.12332E+01 c Velocity[Y] 0.10929E+02 c Velocity[Z] 0.33863E+02 c Pressure 0.75932E-01 8 0.91852E-08 0.25014E+07 0.41629E+02 c k 0.24658E+04 1 0.17462E-05 0.10266E+06 0.16188E+04 c omega 0.81516E+09 1 0.41460E-08 0.31567E+12 0.41140E+02 c TotEner 0.24222E+06 1 0.11105E-05 0.51663E+07 0.24745E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10369E+02 0.25975E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9759e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.52 227.52 0.0017863 0.0010409 v Velocity[Y] -0.13002 701.9 250.54 81.034 v Velocity[Z] -19.181 364.84 25.144 1.9684 v ǁVelocityǁ 0.22549 701.9 260.24 83.774 v Pressure 49945 1.1024e+05 1.0353e+05 1.0416e+05 v k 1.1782e-08 42486 911.66 355.39 v omega 154.36 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 90846 6.2951e+05 3.4161e+05 2.4855e+05 v temperature 61.801 533.95 397.89 337.2 v Density 0.38904 4.9059 0.94901 1.0902 v TurbVisc 8.7735e-19 0.064114 0.010071 0.028644 v CourantNb 1.3179e-05 43.579 0.39246 0.0075982 v FourierNb 4.5101e-05 205.27 1.8332 0.090659 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 61.897 533.95 402.71 421.89 v Boundary Density 0.38914 4.9001 0.98994 0.89868 v Yplus 0 45.425 2.4504 0.95825 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8441e-05 44.245 0.48263 0.010626 INSTANT 0.159111919E-01 TIME STEP NUMBER 30168 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.629838423E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560997905E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124443172E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10340E+01 0.58198E+02 Friction velocity uk : 0.10340E+01 0.58198E+02 Dimensionless distance yplus : 0.20552E-01 0.45452E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14435E-01 0.12558E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60117E+03 2 0.24108E-06 0.46251E+02 0.16423E+03 c Velocity[X] 0.12271E+01 c Velocity[Y] 0.10920E+02 c Velocity[Z] 0.34104E+02 c Pressure 0.75936E-01 8 0.93847E-08 0.25260E+07 0.41832E+02 c k 0.24662E+04 1 0.17630E-05 0.10369E+06 0.16267E+04 c omega 0.81516E+09 1 0.42217E-08 0.30647E+12 0.40536E+02 c TotEner 0.24223E+06 1 0.11104E-05 0.51878E+07 0.24796E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10456E+02 0.26085E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9755e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.55 227.55 0.0017863 0.0010439 v Velocity[Y] -0.13002 701.9 250.54 81.035 v Velocity[Z] -19.18 364.96 25.149 1.9686 v ǁVelocityǁ 0.22557 701.9 260.24 83.775 v Pressure 49929 1.1024e+05 1.0353e+05 1.0416e+05 v k 1.1782e-08 42505 911.7 355.39 v omega 154.37 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 90775 6.2951e+05 3.4161e+05 2.4855e+05 v temperature 61.704 533.95 397.89 337.2 v Density 0.38893 4.9118 0.94901 1.0902 v TurbVisc 8.7732e-19 0.064114 0.010071 0.028644 v CourantNb 1.3179e-05 43.587 0.39252 0.0075983 v FourierNb 4.5103e-05 205.22 1.833 0.09066 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 61.801 533.95 402.71 421.89 v Boundary Density 0.38904 4.9059 0.99001 0.8987 v Yplus 0 45.452 2.4505 0.95834 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8443e-05 44.252 0.4827 0.010626 INSTANT 0.159114549E-01 TIME STEP NUMBER 30169 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.629542372E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560995077E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124452296E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10339E+01 0.58202E+02 Friction velocity uk : 0.10339E+01 0.58202E+02 Dimensionless distance yplus : 0.20552E-01 0.45479E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14434E-01 0.12559E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60117E+03 2 0.24097E-06 0.46499E+02 0.16466E+03 c Velocity[X] 0.12211E+01 c Velocity[Y] 0.10925E+02 c Velocity[Z] 0.34353E+02 c Pressure 0.75940E-01 8 0.91324E-08 0.25512E+07 0.42041E+02 c k 0.24665E+04 1 0.17804E-05 0.10478E+06 0.16351E+04 c omega 0.81516E+09 1 0.42428E-08 0.33270E+12 0.42235E+02 c TotEner 0.24223E+06 1 0.11104E-05 0.52140E+07 0.24858E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10547E+02 0.26198E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.975e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.57 227.57 0.0017864 0.001047 v Velocity[Y] -0.13001 701.9 250.54 81.036 v Velocity[Z] -19.18 365.08 25.154 1.9688 v ǁVelocityǁ 0.22564 701.9 260.24 83.776 v Pressure 49913 1.1024e+05 1.0353e+05 1.0416e+05 v k 1.1781e-08 42523 911.74 355.39 v omega 154.37 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 90704 6.2951e+05 3.4161e+05 2.4855e+05 v temperature 61.607 533.95 397.89 337.21 v Density 0.38883 4.9176 0.949 1.0902 v TurbVisc 8.7729e-19 0.064114 0.010071 0.028644 v CourantNb 1.318e-05 43.595 0.39259 0.0075985 v FourierNb 4.5104e-05 205.16 1.8328 0.090661 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 61.704 533.95 402.7 421.89 v Boundary Density 0.38893 4.9118 0.99009 0.89872 v Yplus 0 45.479 2.4506 0.95842 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8444e-05 44.259 0.48277 0.010626 INSTANT 0.159117180E-01 TIME STEP NUMBER 30170 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.629274730E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560992062E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124460872E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10339E+01 0.58206E+02 Friction velocity uk : 0.10339E+01 0.58206E+02 Dimensionless distance yplus : 0.20552E-01 0.45506E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14434E-01 0.12561E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60117E+03 2 0.24086E-06 0.46748E+02 0.16510E+03 c Velocity[X] 0.12154E+01 c Velocity[Y] 0.10925E+02 c Velocity[Z] 0.34608E+02 c Pressure 0.75944E-01 8 0.89986E-08 0.25769E+07 0.42252E+02 c k 0.24669E+04 1 0.17977E-05 0.10586E+06 0.16433E+04 c omega 0.81516E+09 1 0.54093E-08 0.51030E+12 0.52307E+02 c TotEner 0.24223E+06 1 0.11104E-05 0.52394E+07 0.24919E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10640E+02 0.26313E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9745e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.6 227.6 0.0017865 0.00105 v Velocity[Y] -0.13001 701.9 250.54 81.037 v Velocity[Z] -19.179 365.21 25.159 1.969 v ǁVelocityǁ 0.22572 701.9 260.25 83.777 v Pressure 49897 1.1024e+05 1.0353e+05 1.0416e+05 v k 1.1781e-08 42542 911.78 355.39 v omega 154.38 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 90633 6.295e+05 3.4162e+05 2.4855e+05 v temperature 61.509 533.95 397.89 337.21 v Density 0.38872 4.9236 0.949 1.0902 v TurbVisc 8.7727e-19 0.064114 0.010071 0.028644 v CourantNb 1.3181e-05 43.603 0.39265 0.0075986 v FourierNb 4.5105e-05 205.11 1.8326 0.090662 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 61.607 533.95 402.69 421.89 v Boundary Density 0.38883 4.9176 0.99016 0.89873 v Yplus 0 45.506 2.4506 0.9585 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8445e-05 44.266 0.48283 0.010626 INSTANT 0.159119810E-01 TIME STEP NUMBER 30171 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.629036339E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560988870E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124468901E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10339E+01 0.58209E+02 Friction velocity uk : 0.10339E+01 0.58209E+02 Dimensionless distance yplus : 0.20552E-01 0.45533E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14434E-01 0.12562E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60117E+03 2 0.24075E-06 0.47008E+02 0.16556E+03 c Velocity[X] 0.12098E+01 c Velocity[Y] 0.10926E+02 c Velocity[Z] 0.34872E+02 c Pressure 0.75948E-01 8 0.86489E-08 0.26034E+07 0.42469E+02 c k 0.24672E+04 1 0.18152E-05 0.10696E+06 0.16517E+04 c omega 0.81516E+09 1 0.53407E-08 0.46088E+12 0.49709E+02 c TotEner 0.24223E+06 1 0.11104E-05 0.52666E+07 0.24984E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10735E+02 0.26429E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9741e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.63 227.63 0.0017865 0.001053 v Velocity[Y] -0.13001 701.9 250.54 81.038 v Velocity[Z] -19.179 365.33 25.164 1.9692 v ǁVelocityǁ 0.22579 701.9 260.25 83.778 v Pressure 49881 1.1024e+05 1.0352e+05 1.0416e+05 v k 1.1781e-08 42561 911.82 355.39 v omega 154.38 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 90561 6.295e+05 3.4162e+05 2.4855e+05 v temperature 61.41 533.95 397.89 337.21 v Density 0.38862 4.9296 0.94899 1.0902 v TurbVisc 8.7724e-19 0.064114 0.010071 0.028645 v CourantNb 1.3181e-05 43.61 0.39272 0.0075988 v FourierNb 4.5107e-05 205.06 1.8324 0.090663 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 61.509 533.95 402.69 421.89 v Boundary Density 0.38872 4.9236 0.99024 0.89875 v Yplus 0 45.533 2.4507 0.95859 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8446e-05 44.273 0.4829 0.010626 INSTANT 0.159122440E-01 TIME STEP NUMBER 30172 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.628828009E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560985511E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124476383E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10339E+01 0.58213E+02 Friction velocity uk : 0.10339E+01 0.58213E+02 Dimensionless distance yplus : 0.20552E-01 0.45560E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14434E-01 0.12564E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60117E+03 2 0.24064E-06 0.47278E+02 0.16603E+03 c Velocity[X] 0.12045E+01 c Velocity[Y] 0.10930E+02 c Velocity[Z] 0.35143E+02 c Pressure 0.75952E-01 8 0.86658E-08 0.26305E+07 0.42689E+02 c k 0.24676E+04 1 0.18333E-05 0.10815E+06 0.16607E+04 c omega 0.81516E+09 1 0.47867E-08 0.37370E+12 0.44762E+02 c TotEner 0.24223E+06 1 0.11104E-05 0.52954E+07 0.25052E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10831E+02 0.26549E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9736e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.65 227.65 0.0017866 0.001056 v Velocity[Y] -0.13001 701.9 250.54 81.039 v Velocity[Z] -19.178 365.45 25.169 1.9694 v ǁVelocityǁ 0.22586 701.9 260.26 83.779 v Pressure 49865 1.1024e+05 1.0352e+05 1.0416e+05 v k 1.178e-08 42580 911.86 355.39 v omega 154.39 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 90489 6.295e+05 3.4162e+05 2.4855e+05 v temperature 61.311 533.95 397.88 337.21 v Density 0.38851 4.9357 0.94899 1.0902 v TurbVisc 8.7721e-19 0.064114 0.010071 0.028645 v CourantNb 1.3182e-05 43.618 0.39279 0.0075989 v FourierNb 4.5108e-05 205.01 1.8322 0.090664 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 61.41 533.95 402.68 421.89 v Boundary Density 0.38862 4.9296 0.99032 0.89876 v Yplus 0 45.56 2.4508 0.95867 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8446e-05 44.279 0.48297 0.010627 INSTANT 0.159125070E-01 TIME STEP NUMBER 30173 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.628650516E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560982002E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124483316E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10339E+01 0.58216E+02 Friction velocity uk : 0.10339E+01 0.58216E+02 Dimensionless distance yplus : 0.20551E-01 0.45588E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14434E-01 0.12565E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60118E+03 2 0.24053E-06 0.47562E+02 0.16653E+03 c Velocity[X] 0.11993E+01 c Velocity[Y] 0.10942E+02 c Velocity[Z] 0.35421E+02 c Pressure 0.75956E-01 8 0.88967E-08 0.26582E+07 0.42913E+02 c k 0.24679E+04 1 0.18521E-05 0.10938E+06 0.16700E+04 c omega 0.81516E+09 1 0.44679E-08 0.33349E+12 0.42285E+02 c TotEner 0.24223E+06 1 0.11105E-05 0.53261E+07 0.25124E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10931E+02 0.26671E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9732e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.68 227.68 0.0017869 0.001059 v Velocity[Y] -0.13 701.9 250.54 81.04 v Velocity[Z] -19.178 365.57 25.174 1.9696 v ǁVelocityǁ 0.22594 701.9 260.26 83.78 v Pressure 49849 1.1024e+05 1.0352e+05 1.0416e+05 v k 1.178e-08 42599 911.9 355.39 v omega 154.39 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 90416 6.295e+05 3.4162e+05 2.4855e+05 v temperature 61.211 533.95 397.88 337.21 v Density 0.38841 4.9418 0.94898 1.0902 v TurbVisc 8.7719e-19 0.064114 0.010071 0.028645 v CourantNb 1.3182e-05 43.626 0.39285 0.007599 v FourierNb 4.511e-05 204.96 1.832 0.090665 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 61.311 533.95 402.67 421.88 v Boundary Density 0.38851 4.9357 0.99039 0.89878 v Yplus 0 45.588 2.4509 0.95876 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8447e-05 44.286 0.48303 0.010627 INSTANT 0.159127701E-01 TIME STEP NUMBER 30174 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.628504604E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560978364E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124489700E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10339E+01 0.58220E+02 Friction velocity uk : 0.10339E+01 0.58220E+02 Dimensionless distance yplus : 0.20551E-01 0.45616E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14434E-01 0.12566E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60118E+03 2 0.24043E-06 0.47890E+02 0.16710E+03 c Velocity[X] 0.11943E+01 c Velocity[Y] 0.10987E+02 c Velocity[Z] 0.35708E+02 c Pressure 0.75959E-01 8 0.95863E-08 0.26864E+07 0.43141E+02 c k 0.24683E+04 1 0.18719E-05 0.11070E+06 0.16798E+04 c omega 0.81516E+09 1 0.44087E-08 0.40883E+12 0.46818E+02 c TotEner 0.24223E+06 1 0.11107E-05 0.53659E+07 0.25218E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11036E+02 0.26798E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9727e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.7 227.7 0.001787 0.001062 v Velocity[Y] -0.13 701.9 250.54 81.041 v Velocity[Z] -19.177 365.7 25.179 1.9698 v ǁVelocityǁ 0.22601 701.9 260.26 83.78 v Pressure 49833 1.1024e+05 1.0352e+05 1.0416e+05 v k 1.178e-08 42618 911.94 355.39 v omega 154.4 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 90343 6.295e+05 3.4162e+05 2.4855e+05 v temperature 61.111 533.95 397.88 337.21 v Density 0.3883 4.9479 0.94898 1.0902 v TurbVisc 8.7716e-19 0.064114 0.010071 0.028645 v CourantNb 1.3183e-05 43.634 0.39292 0.0075992 v FourierNb 4.5112e-05 204.91 1.8317 0.090666 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 61.211 533.95 402.67 421.88 v Boundary Density 0.38841 4.9418 0.99047 0.8988 v Yplus 0 45.616 2.451 0.95884 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8448e-05 44.293 0.4831 0.010627 INSTANT 0.159130331E-01 TIME STEP NUMBER 30175 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.628390981E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560974615E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124495535E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10339E+01 0.58224E+02 Friction velocity uk : 0.10339E+01 0.58224E+02 Dimensionless distance yplus : 0.20551E-01 0.45644E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14434E-01 0.12568E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60118E+03 2 0.24032E-06 0.48161E+02 0.16757E+03 c Velocity[X] 0.11896E+01 c Velocity[Y] 0.10969E+02 c Velocity[Z] 0.36002E+02 c Pressure 0.75963E-01 8 0.99736E-08 0.27154E+07 0.43372E+02 c k 0.24687E+04 1 0.18903E-05 0.11185E+06 0.16884E+04 c omega 0.81516E+09 1 0.42249E-08 0.35489E+12 0.43620E+02 c TotEner 0.24224E+06 1 0.11107E-05 0.53886E+07 0.25271E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11136E+02 0.26920E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9723e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.73 227.73 0.0017872 0.001065 v Velocity[Y] -0.13 701.9 250.54 81.042 v Velocity[Z] -19.177 365.82 25.184 1.97 v ǁVelocityǁ 0.22608 701.9 260.27 83.781 v Pressure 49816 1.1024e+05 1.0352e+05 1.0416e+05 v k 1.1779e-08 42638 911.98 355.38 v omega 154.4 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 90269 6.295e+05 3.4162e+05 2.4855e+05 v temperature 61.009 533.95 397.88 337.21 v Density 0.3882 4.9542 0.94898 1.0902 v TurbVisc 8.7714e-19 0.064113 0.010071 0.028645 v CourantNb 1.3183e-05 43.642 0.39298 0.0075993 v FourierNb 4.5113e-05 204.86 1.8315 0.090667 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 61.111 533.95 402.66 421.88 v Boundary Density 0.3883 4.9479 0.99055 0.89881 v Yplus 0 45.644 2.451 0.95893 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8448e-05 44.3 0.48317 0.010627 INSTANT 0.159132961E-01 TIME STEP NUMBER 30176 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.628310319E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560970763E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124500817E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10339E+01 0.58227E+02 Friction velocity uk : 0.10339E+01 0.58227E+02 Dimensionless distance yplus : 0.20551E-01 0.45673E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14434E-01 0.12569E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60118E+03 2 0.24022E-06 0.48433E+02 0.16804E+03 c Velocity[X] 0.11849E+01 c Velocity[Y] 0.10943E+02 c Velocity[Z] 0.36304E+02 c Pressure 0.75967E-01 8 0.96606E-08 0.27448E+07 0.43607E+02 c k 0.24690E+04 1 0.19086E-05 0.11303E+06 0.16971E+04 c omega 0.81516E+09 1 0.44340E-08 0.37571E+12 0.44882E+02 c TotEner 0.24224E+06 1 0.11108E-05 0.54115E+07 0.25325E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11239E+02 0.27044E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9718e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.76 227.76 0.0017876 0.0010679 v Velocity[Y] -0.12999 701.9 250.54 81.043 v Velocity[Z] -19.176 365.94 25.189 1.9702 v ǁVelocityǁ 0.22615 701.9 260.27 83.782 v Pressure 49800 1.1024e+05 1.0352e+05 1.0416e+05 v k 1.1779e-08 42657 912.02 355.38 v omega 154.41 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 90194 6.295e+05 3.4162e+05 2.4855e+05 v temperature 60.907 533.95 397.88 337.21 v Density 0.38809 4.9604 0.94897 1.0902 v TurbVisc 8.7711e-19 0.064113 0.010071 0.028645 v CourantNb 1.3184e-05 43.65 0.39305 0.0075995 v FourierNb 4.5115e-05 204.81 1.8313 0.090668 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 61.009 533.95 402.65 421.88 v Boundary Density 0.3882 4.9542 0.99063 0.89883 v Yplus 0 45.673 2.4511 0.95902 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8449e-05 44.306 0.48323 0.010627 INSTANT 0.159135592E-01 TIME STEP NUMBER 30177 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.628263255E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560966814E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124505547E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10339E+01 0.58231E+02 Friction velocity uk : 0.10339E+01 0.58231E+02 Dimensionless distance yplus : 0.20551E-01 0.45701E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14434E-01 0.12571E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60118E+03 2 0.24011E-06 0.48718E+02 0.16854E+03 c Velocity[X] 0.11804E+01 c Velocity[Y] 0.10923E+02 c Velocity[Z] 0.36615E+02 c Pressure 0.75971E-01 8 0.99461E-08 0.27747E+07 0.43844E+02 c k 0.24694E+04 1 0.19271E-05 0.11425E+06 0.17061E+04 c omega 0.81516E+09 1 0.37619E-08 0.26319E+12 0.37564E+02 c TotEner 0.24224E+06 1 0.11108E-05 0.54368E+07 0.25384E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11345E+02 0.27170E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9713e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.78 227.78 0.0017881 0.0010709 v Velocity[Y] -0.12999 701.9 250.54 81.044 v Velocity[Z] -19.176 366.07 25.194 1.9704 v ǁVelocityǁ 0.22623 701.9 260.27 83.783 v Pressure 49784 1.1024e+05 1.0352e+05 1.0416e+05 v k 1.1779e-08 42676 912.06 355.38 v omega 154.41 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 90119 6.295e+05 3.4162e+05 2.4855e+05 v temperature 60.805 533.95 397.88 337.21 v Density 0.38799 4.9668 0.94897 1.0902 v TurbVisc 8.7709e-19 0.064113 0.010072 0.028646 v CourantNb 1.3184e-05 43.658 0.39311 0.0075996 v FourierNb 4.5116e-05 204.76 1.8311 0.09067 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 60.907 533.95 402.65 421.88 v Boundary Density 0.38809 4.9604 0.99071 0.89885 v Yplus 0 45.701 2.4512 0.9591 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8449e-05 44.313 0.4833 0.010628 INSTANT 0.159138222E-01 TIME STEP NUMBER 30178 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.628250388E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560962777E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124509722E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10339E+01 0.58234E+02 Friction velocity uk : 0.10339E+01 0.58234E+02 Dimensionless distance yplus : 0.20551E-01 0.45730E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14433E-01 0.12572E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60119E+03 2 0.24001E-06 0.49032E+02 0.16908E+03 c Velocity[X] 0.11761E+01 c Velocity[Y] 0.10922E+02 c Velocity[Z] 0.36934E+02 c Pressure 0.75975E-01 9 0.94369E-08 0.28053E+07 0.44085E+02 c k 0.24698E+04 1 0.19467E-05 0.11558E+06 0.17158E+04 c omega 0.81516E+09 1 0.40608E-08 0.27831E+12 0.38628E+02 c TotEner 0.24224E+06 1 0.11110E-05 0.54679E+07 0.25456E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11454E+02 0.27301E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9709e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.81 227.81 0.0017885 0.0010739 v Velocity[Y] -0.12999 701.9 250.54 81.045 v Velocity[Z] -19.175 366.19 25.199 1.9706 v ǁVelocityǁ 0.2263 701.9 260.28 83.784 v Pressure 49768 1.1024e+05 1.0352e+05 1.0416e+05 v k 1.1778e-08 42696 912.1 355.38 v omega 154.42 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 90044 6.295e+05 3.4162e+05 2.4855e+05 v temperature 60.701 533.95 397.88 337.21 v Density 0.38788 4.9732 0.94896 1.0902 v TurbVisc 8.7706e-19 0.064113 0.010072 0.028646 v CourantNb 1.3184e-05 43.666 0.39318 0.0075997 v FourierNb 4.5118e-05 204.71 1.8309 0.090671 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 60.805 533.95 402.64 421.88 v Boundary Density 0.38799 4.9668 0.99079 0.89887 v Yplus 0 45.73 2.4513 0.95919 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.845e-05 44.32 0.48337 0.010628 INSTANT 0.159140852E-01 TIME STEP NUMBER 30179 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.628272281E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560958659E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124513339E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10339E+01 0.58238E+02 Friction velocity uk : 0.10339E+01 0.58238E+02 Dimensionless distance yplus : 0.20550E-01 0.45759E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14433E-01 0.12574E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60119E+03 2 0.23990E-06 0.49343E+02 0.16961E+03 c Velocity[X] 0.11719E+01 c Velocity[Y] 0.10910E+02 c Velocity[Z] 0.37261E+02 c Pressure 0.75979E-01 9 0.96636E-08 0.28369E+07 0.44332E+02 c k 0.24702E+04 1 0.19662E-05 0.11690E+06 0.17254E+04 c omega 0.81517E+09 1 0.46530E-08 0.43792E+12 0.48455E+02 c TotEner 0.24224E+06 1 0.11111E-05 0.54974E+07 0.25525E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11565E+02 0.27433E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9704e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.84 227.83 0.0017888 0.0010768 v Velocity[Y] -0.12999 701.9 250.54 81.045 v Velocity[Z] -19.175 366.31 25.204 1.9708 v ǁVelocityǁ 0.22637 701.9 260.28 83.785 v Pressure 49752 1.1024e+05 1.0352e+05 1.0416e+05 v k 1.1778e-08 42715 912.15 355.38 v omega 154.42 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 89968 6.295e+05 3.4162e+05 2.4855e+05 v temperature 60.597 533.95 397.87 337.21 v Density 0.38778 4.9797 0.94896 1.0902 v TurbVisc 8.7704e-19 0.064113 0.010072 0.028646 v CourantNb 1.3184e-05 43.674 0.39324 0.0075999 v FourierNb 4.512e-05 204.66 1.8307 0.090672 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 60.701 533.95 402.63 421.88 v Boundary Density 0.38788 4.9732 0.99088 0.89888 v Yplus 0 45.759 2.4514 0.95928 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.845e-05 44.327 0.48343 0.010628 INSTANT 0.159143482E-01 TIME STEP NUMBER 30180 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.628329457E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560954465E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124516397E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10339E+01 0.58242E+02 Friction velocity uk : 0.10339E+01 0.58242E+02 Dimensionless distance yplus : 0.20550E-01 0.45789E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14433E-01 0.12575E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60119E+03 2 0.23980E-06 0.49686E+02 0.17020E+03 c Velocity[X] 0.11680E+01 c Velocity[Y] 0.10921E+02 c Velocity[Z] 0.37597E+02 c Pressure 0.75983E-01 9 0.93736E-08 0.28691E+07 0.44583E+02 c k 0.24705E+04 1 0.19865E-05 0.11833E+06 0.17357E+04 c omega 0.81517E+09 1 0.43558E-08 0.35864E+12 0.43850E+02 c TotEner 0.24224E+06 1 0.11113E-05 0.55344E+07 0.25610E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11681E+02 0.27570E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.97e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.86 227.86 0.0017891 0.0010798 v Velocity[Y] -0.12998 701.9 250.54 81.046 v Velocity[Z] -19.174 366.44 25.209 1.971 v ǁVelocityǁ 0.22643 701.9 260.29 83.786 v Pressure 49736 1.1024e+05 1.0351e+05 1.0416e+05 v k 1.1778e-08 42735 912.19 355.38 v omega 154.43 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 89892 6.295e+05 3.4162e+05 2.4855e+05 v temperature 60.492 533.95 397.87 337.21 v Density 0.38767 4.9862 0.94895 1.0902 v TurbVisc 8.7701e-19 0.064113 0.010072 0.028646 v CourantNb 1.3184e-05 43.682 0.39331 0.0076 v FourierNb 4.5122e-05 204.61 1.8305 0.090673 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 60.597 533.95 402.63 421.87 v Boundary Density 0.38778 4.9797 0.99096 0.8989 v Yplus 0 45.789 2.4515 0.95937 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.845e-05 44.334 0.4835 0.010628 INSTANT 0.159146113E-01 TIME STEP NUMBER 30181 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.628422403E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560950192E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124518894E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10339E+01 0.58245E+02 Friction velocity uk : 0.10339E+01 0.58245E+02 Dimensionless distance yplus : 0.20550E-01 0.45819E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14433E-01 0.12577E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60119E+03 2 0.23969E-06 0.50027E+02 0.17078E+03 c Velocity[X] 0.11643E+01 c Velocity[Y] 0.10921E+02 c Velocity[Z] 0.37942E+02 c Pressure 0.75987E-01 9 0.98610E-08 0.29016E+07 0.44835E+02 c k 0.24709E+04 1 0.20073E-05 0.11980E+06 0.17463E+04 c omega 0.81517E+09 1 0.43182E-08 0.32607E+12 0.41812E+02 c TotEner 0.24224E+06 1 0.11115E-05 0.55666E+07 0.25685E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11797E+02 0.27707E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9695e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.89 227.89 0.0017895 0.0010827 v Velocity[Y] -0.12998 701.9 250.54 81.047 v Velocity[Z] -19.174 366.56 25.214 1.9712 v ǁVelocityǁ 0.2265 701.9 260.29 83.787 v Pressure 49720 1.1024e+05 1.0351e+05 1.0416e+05 v k 1.1777e-08 42755 912.23 355.38 v omega 154.43 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 89815 6.295e+05 3.4162e+05 2.4855e+05 v temperature 60.387 533.95 397.87 337.21 v Density 0.38757 4.9928 0.94895 1.0902 v TurbVisc 8.7699e-19 0.064113 0.010072 0.028646 v CourantNb 1.3184e-05 43.69 0.39338 0.0076002 v FourierNb 4.5123e-05 204.56 1.8303 0.090674 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 60.492 533.95 402.62 421.87 v Boundary Density 0.38767 4.9862 0.99104 0.89892 v Yplus 0 45.819 2.4516 0.95946 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.845e-05 44.34 0.48357 0.010628 INSTANT 0.159148743E-01 TIME STEP NUMBER 30182 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.628551566E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560945846E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124520826E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+01 0.58249E+02 Friction velocity uk : 0.10338E+01 0.58249E+02 Dimensionless distance yplus : 0.20550E-01 0.45849E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14433E-01 0.12579E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60119E+03 2 0.23959E-06 0.50374E+02 0.17137E+03 c Velocity[X] 0.11607E+01 c Velocity[Y] 0.10918E+02 c Velocity[Z] 0.38295E+02 c Pressure 0.75991E-01 9 0.98640E-08 0.29351E+07 0.45094E+02 c k 0.24713E+04 1 0.20280E-05 0.12124E+06 0.17566E+04 c omega 0.81517E+09 1 0.41328E-08 0.30785E+12 0.40627E+02 c TotEner 0.24225E+06 1 0.11117E-05 0.56004E+07 0.25762E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11916E+02 0.27846E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9691e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.91 227.91 0.00179 0.0010856 v Velocity[Y] -0.12998 701.9 250.54 81.048 v Velocity[Z] -19.173 366.69 25.219 1.9714 v ǁVelocityǁ 0.22657 701.9 260.29 83.788 v Pressure 49704 1.1024e+05 1.0351e+05 1.0416e+05 v k 1.1777e-08 42774 912.28 355.38 v omega 154.44 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 89737 6.295e+05 3.4162e+05 2.4855e+05 v temperature 60.28 533.95 397.87 337.21 v Density 0.38746 4.9995 0.94895 1.0902 v TurbVisc 8.7696e-19 0.064113 0.010072 0.028646 v CourantNb 1.3184e-05 43.698 0.39344 0.0076003 v FourierNb 4.5125e-05 204.51 1.8301 0.090675 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 60.387 533.95 402.61 421.87 v Boundary Density 0.38757 4.9928 0.99113 0.89894 v Yplus 0 45.849 2.4517 0.95955 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.845e-05 44.347 0.48363 0.010629 INSTANT 0.159151373E-01 TIME STEP NUMBER 30183 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.628717354E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560941418E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124522191E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+01 0.58252E+02 Friction velocity uk : 0.10338E+01 0.58252E+02 Dimensionless distance yplus : 0.20550E-01 0.45879E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14433E-01 0.12580E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60120E+03 2 0.23949E-06 0.50735E+02 0.17198E+03 c Velocity[X] 0.11573E+01 c Velocity[Y] 0.10919E+02 c Velocity[Z] 0.38658E+02 c Pressure 0.75995E-01 10 0.74700E-08 0.29691E+07 0.45354E+02 c k 0.24717E+04 2 0.18396E-06 0.12931E+06 0.18139E+04 c omega 0.81517E+09 1 0.37912E-08 0.25175E+12 0.36739E+02 c TotEner 0.24225E+06 1 0.11120E-05 0.56357E+07 0.25844E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12038E+02 0.27988E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9686e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.94 227.94 0.0017906 0.0010885 v Velocity[Y] -0.12997 701.9 250.54 81.049 v Velocity[Z] -19.173 366.81 25.224 1.9716 v ǁVelocityǁ 0.22664 701.9 260.3 83.789 v Pressure 49688 1.1024e+05 1.0351e+05 1.0416e+05 v k 1.1777e-08 42794 912.33 355.38 v omega 154.44 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 89659 6.295e+05 3.4162e+05 2.4855e+05 v temperature 60.173 533.94 397.87 337.21 v Density 0.38736 5.0062 0.94894 1.0902 v TurbVisc 8.7694e-19 0.064112 0.010072 0.028647 v CourantNb 1.3184e-05 43.706 0.39351 0.0076004 v FourierNb 4.5127e-05 204.46 1.8299 0.090676 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 60.28 533.95 402.6 421.87 v Boundary Density 0.38746 4.9995 0.99122 0.89895 v Yplus 0 45.879 2.4518 0.95964 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.845e-05 44.354 0.4837 0.010629 INSTANT 0.159154004E-01 TIME STEP NUMBER 30184 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.628920136E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560936908E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124522986E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+01 0.58256E+02 Friction velocity uk : 0.10338E+01 0.58256E+02 Dimensionless distance yplus : 0.20550E-01 0.45909E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14433E-01 0.12582E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60120E+03 2 0.23939E-06 0.51099E+02 0.17260E+03 c Velocity[X] 0.11539E+01 c Velocity[Y] 0.10916E+02 c Velocity[Z] 0.39029E+02 c Pressure 0.75999E-01 8 0.95988E-08 0.30040E+07 0.45619E+02 c k 0.24721E+04 2 0.18409E-06 0.13063E+06 0.18230E+04 c omega 0.81517E+09 1 0.39651E-08 0.29929E+12 0.40058E+02 c TotEner 0.24225E+06 1 0.11122E-05 0.56714E+07 0.25925E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12164E+02 0.28134E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9682e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.97 227.97 0.0017912 0.0010914 v Velocity[Y] -0.12997 701.9 250.55 81.05 v Velocity[Z] -19.172 366.93 25.229 1.9718 v ǁVelocityǁ 0.22671 701.9 260.3 83.79 v Pressure 49672 1.1024e+05 1.0351e+05 1.0416e+05 v k 1.1776e-08 42814 912.37 355.38 v omega 154.45 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 89580 6.295e+05 3.4162e+05 2.4855e+05 v temperature 60.065 533.94 397.87 337.21 v Density 0.38725 5.013 0.94894 1.0902 v TurbVisc 8.7691e-19 0.064112 0.010072 0.028647 v CourantNb 1.3184e-05 43.713 0.39357 0.0076006 v FourierNb 4.5129e-05 204.41 1.8297 0.090677 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 60.173 533.94 402.6 421.87 v Boundary Density 0.38736 5.0062 0.9913 0.89897 v Yplus 0 45.909 2.4519 0.95973 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.845e-05 44.361 0.48377 0.010629 INSTANT 0.159156634E-01 TIME STEP NUMBER 30185 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.629160237E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560932297E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124523208E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+01 0.58260E+02 Friction velocity uk : 0.10338E+01 0.58260E+02 Dimensionless distance yplus : 0.20550E-01 0.45940E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14433E-01 0.12583E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60120E+03 2 0.23928E-06 0.51463E+02 0.17321E+03 c Velocity[X] 0.11506E+01 c Velocity[Y] 0.10902E+02 c Velocity[Z] 0.39410E+02 c Pressure 0.76003E-01 8 0.95233E-08 0.30397E+07 0.45890E+02 c k 0.24725E+04 2 0.18438E-06 0.13198E+06 0.18321E+04 c omega 0.81517E+09 1 0.36684E-08 0.27755E+12 0.38576E+02 c TotEner 0.24225E+06 1 0.11125E-05 0.57064E+07 0.26005E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12293E+02 0.28283E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9677e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -227.99 227.99 0.0017918 0.0010943 v Velocity[Y] -0.12997 701.9 250.55 81.051 v Velocity[Z] -19.172 367.06 25.234 1.9719 v ǁVelocityǁ 0.22677 701.9 260.3 83.791 v Pressure 49656 1.1024e+05 1.0351e+05 1.0416e+05 v k 1.1776e-08 42834 912.42 355.38 v omega 154.45 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 89501 6.295e+05 3.4162e+05 2.4855e+05 v temperature 59.957 533.94 397.86 337.21 v Density 0.38715 5.0199 0.94893 1.0902 v TurbVisc 8.7688e-19 0.064111 0.010072 0.028647 v CourantNb 1.3183e-05 43.721 0.39364 0.0076007 v FourierNb 4.5131e-05 204.37 1.8295 0.090678 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 60.065 533.94 402.59 421.87 v Boundary Density 0.38725 5.013 0.99139 0.89899 v Yplus 0 45.94 2.452 0.95982 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8449e-05 44.367 0.48383 0.010629 INSTANT 0.159159264E-01 TIME STEP NUMBER 30186 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.629437947E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560927608E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124522868E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+01 0.58263E+02 Friction velocity uk : 0.10338E+01 0.58263E+02 Dimensionless distance yplus : 0.20549E-01 0.45971E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14433E-01 0.12585E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60120E+03 2 0.23918E-06 0.51849E+02 0.17385E+03 c Velocity[X] 0.11473E+01 c Velocity[Y] 0.10901E+02 c Velocity[Z] 0.39800E+02 c Pressure 0.76007E-01 10 0.73528E-08 0.30760E+07 0.46163E+02 c k 0.24729E+04 2 0.18477E-06 0.13341E+06 0.18419E+04 c omega 0.81517E+09 1 0.38206E-08 0.30957E+12 0.40740E+02 c TotEner 0.24225E+06 1 0.11128E-05 0.57450E+07 0.26093E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12425E+02 0.28434E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9673e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.02 228.02 0.0017926 0.0010972 v Velocity[Y] -0.12997 701.9 250.55 81.052 v Velocity[Z] -19.171 367.18 25.239 1.9721 v ǁVelocityǁ 0.22684 701.9 260.31 83.792 v Pressure 49640 1.1024e+05 1.0351e+05 1.0416e+05 v k 1.1775e-08 42855 912.47 355.38 v omega 154.46 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 89421 6.295e+05 3.4162e+05 2.4855e+05 v temperature 59.847 533.94 397.86 337.21 v Density 0.38704 5.0268 0.94893 1.0902 v TurbVisc 8.7685e-19 0.064111 0.010072 0.028647 v CourantNb 1.3183e-05 43.729 0.3937 0.0076009 v FourierNb 4.5133e-05 204.32 1.8293 0.090679 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 59.957 533.94 402.58 421.87 v Boundary Density 0.38715 5.0199 0.99148 0.89901 v Yplus 0 45.971 2.4521 0.95992 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8449e-05 44.374 0.4839 0.010629 INSTANT 0.159161895E-01 TIME STEP NUMBER 30187 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.629753511E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560922845E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124521963E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+01 0.58267E+02 Friction velocity uk : 0.10338E+01 0.58267E+02 Dimensionless distance yplus : 0.20549E-01 0.46003E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14432E-01 0.12587E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60120E+03 2 0.23908E-06 0.52244E+02 0.17451E+03 c Velocity[X] 0.11440E+01 c Velocity[Y] 0.10899E+02 c Velocity[Z] 0.40200E+02 c Pressure 0.76011E-01 10 0.71872E-08 0.31132E+07 0.46441E+02 c k 0.24733E+04 2 0.18523E-06 0.13492E+06 0.18521E+04 c omega 0.81517E+09 1 0.35802E-08 0.24424E+12 0.36186E+02 c TotEner 0.24225E+06 1 0.11132E-05 0.57846E+07 0.26183E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12561E+02 0.28589E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9668e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.04 228.04 0.0017934 0.0011001 v Velocity[Y] -0.12996 701.9 250.55 81.053 v Velocity[Z] -19.171 367.31 25.244 1.9723 v ǁVelocityǁ 0.2269 701.9 260.31 83.793 v Pressure 49624 1.1024e+05 1.0351e+05 1.0416e+05 v k 1.1775e-08 42875 912.52 355.38 v omega 154.46 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 89341 6.295e+05 3.4162e+05 2.4855e+05 v temperature 59.737 533.94 397.86 337.21 v Density 0.38694 5.0338 0.94893 1.0902 v TurbVisc 8.7682e-19 0.06411 0.010072 0.028647 v CourantNb 1.3183e-05 43.737 0.39377 0.007601 v FourierNb 4.5135e-05 204.27 1.8291 0.09068 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 59.847 533.94 402.58 421.86 v Boundary Density 0.38704 5.0268 0.99157 0.89903 v Yplus 0 46.003 2.4522 0.96001 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8448e-05 44.381 0.48397 0.01063 INSTANT 0.159164525E-01 TIME STEP NUMBER 30188 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.630107135E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560917998E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124520486E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+01 0.58270E+02 Friction velocity uk : 0.10338E+01 0.58270E+02 Dimensionless distance yplus : 0.20549E-01 0.46035E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14432E-01 0.12588E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60120E+03 2 0.23898E-06 0.52655E+02 0.17520E+03 c Velocity[X] 0.11407E+01 c Velocity[Y] 0.10903E+02 c Velocity[Z] 0.40611E+02 c Pressure 0.76015E-01 10 0.73507E-08 0.31511E+07 0.46723E+02 c k 0.24738E+04 2 0.18575E-06 0.13650E+06 0.18626E+04 c omega 0.81517E+09 1 0.39829E-08 0.28681E+12 0.39214E+02 c TotEner 0.24225E+06 1 0.11136E-05 0.58269E+07 0.26278E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12699E+02 0.28746E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9664e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.07 228.07 0.0017944 0.001103 v Velocity[Y] -0.12996 701.9 250.55 81.054 v Velocity[Z] -19.17 367.43 25.249 1.9725 v ǁVelocityǁ 0.22697 701.9 260.32 83.793 v Pressure 49608 1.1024e+05 1.035e+05 1.0416e+05 v k 1.1775e-08 42895 912.57 355.38 v omega 154.47 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 89260 6.295e+05 3.4162e+05 2.4855e+05 v temperature 59.626 533.94 397.86 337.21 v Density 0.38683 5.0409 0.94892 1.0902 v TurbVisc 8.768e-19 0.06411 0.010073 0.028647 v CourantNb 1.3182e-05 43.745 0.39383 0.0076011 v FourierNb 4.5137e-05 204.23 1.8289 0.090681 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 59.737 533.94 402.57 421.86 v Boundary Density 0.38694 5.0338 0.99166 0.89905 v Yplus 0 46.035 2.4523 0.96011 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8448e-05 44.388 0.48403 0.01063 INSTANT 0.159167155E-01 TIME STEP NUMBER 30189 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.630498984E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560913083E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124518434E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+01 0.58274E+02 Friction velocity uk : 0.10338E+01 0.58274E+02 Dimensionless distance yplus : 0.20549E-01 0.46067E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14432E-01 0.12590E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60121E+03 2 0.23887E-06 0.53075E+02 0.17589E+03 c Velocity[X] 0.11376E+01 c Velocity[Y] 0.10906E+02 c Velocity[Z] 0.41031E+02 c Pressure 0.76019E-01 10 0.72701E-08 0.31899E+07 0.47010E+02 c k 0.24742E+04 2 0.18633E-06 0.13810E+06 0.18733E+04 c omega 0.81517E+09 1 0.36846E-08 0.23571E+12 0.35549E+02 c TotEner 0.24226E+06 1 0.11140E-05 0.58700E+07 0.26375E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12841E+02 0.28906E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9659e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.1 228.1 0.0017955 0.0011058 v Velocity[Y] -0.12996 701.9 250.55 81.055 v Velocity[Z] -19.17 367.56 25.254 1.9727 v ǁVelocityǁ 0.22703 701.9 260.32 83.794 v Pressure 49592 1.1024e+05 1.035e+05 1.0416e+05 v k 1.1774e-08 42916 912.62 355.37 v omega 154.47 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 89178 6.295e+05 3.4162e+05 2.4855e+05 v temperature 59.515 533.94 397.86 337.21 v Density 0.38673 5.0481 0.94892 1.0902 v TurbVisc 8.7677e-19 0.064109 0.010073 0.028648 v CourantNb 1.3182e-05 43.753 0.3939 0.0076013 v FourierNb 4.5139e-05 204.18 1.8287 0.090682 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 59.626 533.94 402.56 421.86 v Boundary Density 0.38683 5.0409 0.99175 0.89907 v Yplus 0 46.067 2.4524 0.9602 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8447e-05 44.394 0.4841 0.01063 INSTANT 0.159169786E-01 TIME STEP NUMBER 30190 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.630929180E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560908121E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124515800E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+01 0.58278E+02 Friction velocity uk : 0.10338E+01 0.58278E+02 Dimensionless distance yplus : 0.20549E-01 0.46099E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14432E-01 0.12592E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60121E+03 2 0.23877E-06 0.53502E+02 0.17660E+03 c Velocity[X] 0.11347E+01 c Velocity[Y] 0.10906E+02 c Velocity[Z] 0.41462E+02 c Pressure 0.76023E-01 10 0.71204E-08 0.32292E+07 0.47299E+02 c k 0.24746E+04 2 0.18695E-06 0.13976E+06 0.18844E+04 c omega 0.81517E+09 1 0.39683E-08 0.27393E+12 0.38323E+02 c TotEner 0.24226E+06 1 0.11144E-05 0.59127E+07 0.26471E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12985E+02 0.29068E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9655e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.12 228.12 0.0017967 0.0011087 v Velocity[Y] -0.12996 701.9 250.55 81.056 v Velocity[Z] -19.169 367.68 25.26 1.9729 v ǁVelocityǁ 0.22709 701.9 260.32 83.795 v Pressure 49576 1.1024e+05 1.035e+05 1.0416e+05 v k 1.1774e-08 42936 912.67 355.37 v omega 154.48 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 89096 6.295e+05 3.4162e+05 2.4855e+05 v temperature 59.402 533.94 397.86 337.21 v Density 0.38662 5.0553 0.94891 1.0902 v TurbVisc 8.7675e-19 0.064109 0.010073 0.028648 v CourantNb 1.3181e-05 43.761 0.39397 0.0076014 v FourierNb 4.5141e-05 204.13 1.8285 0.090683 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 59.515 533.94 402.55 421.86 v Boundary Density 0.38673 5.0481 0.99184 0.89909 v Yplus 0 46.099 2.4525 0.9603 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8446e-05 44.401 0.48417 0.01063 INSTANT 0.159172416E-01 TIME STEP NUMBER 30191 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.631397805E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560903128E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124512580E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+01 0.58281E+02 Friction velocity uk : 0.10338E+01 0.58281E+02 Dimensionless distance yplus : 0.20549E-01 0.46132E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14432E-01 0.12593E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60121E+03 2 0.23867E-06 0.53931E+02 0.17730E+03 c Velocity[X] 0.11320E+01 c Velocity[Y] 0.10897E+02 c Velocity[Z] 0.41902E+02 c Pressure 0.76027E-01 10 0.68559E-08 0.32695E+07 0.47593E+02 c k 0.24750E+04 2 0.18761E-06 0.14143E+06 0.18954E+04 c omega 0.81517E+09 1 0.50010E-08 0.39905E+12 0.46254E+02 c TotEner 0.24226E+06 1 0.11149E-05 0.59547E+07 0.26565E+02 c temperature 0.00000E+00 0 0.00000E+00 0.13132E+02 0.29231E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.965e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.15 228.15 0.001798 0.0011116 v Velocity[Y] -0.12995 701.9 250.55 81.057 v Velocity[Z] -19.169 367.81 25.265 1.9731 v ǁVelocityǁ 0.22716 701.9 260.33 83.796 v Pressure 49559 1.1024e+05 1.035e+05 1.0416e+05 v k 1.1774e-08 42957 912.72 355.37 v omega 154.48 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 89013 6.295e+05 3.4162e+05 2.4855e+05 v temperature 59.288 533.94 397.86 337.21 v Density 0.38652 5.0626 0.94891 1.0902 v TurbVisc 8.7672e-19 0.064108 0.010073 0.028648 v CourantNb 1.318e-05 43.769 0.39403 0.0076016 v FourierNb 4.5143e-05 204.09 1.8283 0.090684 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 59.402 533.94 402.55 421.86 v Boundary Density 0.38662 5.0553 0.99193 0.89911 v Yplus 0 46.132 2.4526 0.9604 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8445e-05 44.408 0.48423 0.01063 INSTANT 0.159175046E-01 TIME STEP NUMBER 30192 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.631904898E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560898116E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124508768E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+01 0.58285E+02 Friction velocity uk : 0.10338E+01 0.58285E+02 Dimensionless distance yplus : 0.20549E-01 0.46165E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14432E-01 0.12595E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60121E+03 2 0.23857E-06 0.54377E+02 0.17803E+03 c Velocity[X] 0.11295E+01 c Velocity[Y] 0.10894E+02 c Velocity[Z] 0.42353E+02 c Pressure 0.76031E-01 8 0.90928E-08 0.33104E+07 0.47890E+02 c k 0.24755E+04 2 0.18830E-06 0.14316E+06 0.19067E+04 c omega 0.81517E+09 1 0.51284E-08 0.38506E+12 0.45437E+02 c TotEner 0.24226E+06 1 0.11153E-05 0.59988E+07 0.26663E+02 c temperature 0.00000E+00 0 0.00000E+00 0.13281E+02 0.29397E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9646e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.17 228.17 0.0017996 0.0011144 v Velocity[Y] -0.12995 701.9 250.55 81.058 v Velocity[Z] -19.168 367.93 25.27 1.9733 v ǁVelocityǁ 0.22722 701.9 260.33 83.797 v Pressure 49543 1.1024e+05 1.035e+05 1.0416e+05 v k 1.1773e-08 42977 912.77 355.37 v omega 154.49 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 88929 6.295e+05 3.4162e+05 2.4855e+05 v temperature 59.174 533.94 397.85 337.21 v Density 0.38641 5.07 0.9489 1.0902 v TurbVisc 8.767e-19 0.064108 0.010073 0.028648 v CourantNb 1.318e-05 43.777 0.3941 0.0076017 v FourierNb 4.5145e-05 204.04 1.8281 0.090685 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 59.288 533.94 402.54 421.86 v Boundary Density 0.38652 5.0626 0.99203 0.89913 v Yplus 0 46.165 2.4527 0.96049 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8444e-05 44.415 0.4843 0.01063 INSTANT 0.159177677E-01 TIME STEP NUMBER 30193 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.632450458E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560893097E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124504360E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+01 0.58288E+02 Friction velocity uk : 0.10338E+01 0.58288E+02 Dimensionless distance yplus : 0.20548E-01 0.46198E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14432E-01 0.12597E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60121E+03 2 0.23847E-06 0.54836E+02 0.17878E+03 c Velocity[X] 0.11273E+01 c Velocity[Y] 0.10894E+02 c Velocity[Z] 0.42815E+02 c Pressure 0.76035E-01 8 0.89389E-08 0.33524E+07 0.48193E+02 c k 0.24759E+04 2 0.18903E-06 0.14498E+06 0.19186E+04 c omega 0.81517E+09 1 0.50207E-08 0.45455E+12 0.49366E+02 c TotEner 0.24226E+06 1 0.11158E-05 0.60453E+07 0.26766E+02 c temperature 0.00000E+00 0 0.00000E+00 0.13435E+02 0.29567E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9641e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.2 228.2 0.0018013 0.0011173 v Velocity[Y] -0.12995 701.9 250.55 81.059 v Velocity[Z] -19.168 368.06 25.275 1.9735 v ǁVelocityǁ 0.22728 701.9 260.34 83.798 v Pressure 49527 1.1024e+05 1.035e+05 1.0416e+05 v k 1.1773e-08 42998 912.82 355.37 v omega 154.49 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 88845 6.295e+05 3.4162e+05 2.4855e+05 v temperature 59.059 533.94 397.85 337.21 v Density 0.38631 5.0775 0.9489 1.0902 v TurbVisc 8.7667e-19 0.064107 0.010073 0.028648 v CourantNb 1.3179e-05 43.785 0.39416 0.0076018 v FourierNb 4.5147e-05 203.99 1.8279 0.090686 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 59.174 533.94 402.53 421.86 v Boundary Density 0.38641 5.07 0.99212 0.89915 v Yplus 0 46.198 2.4528 0.96059 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8443e-05 44.421 0.48437 0.010631 INSTANT 0.159180307E-01 TIME STEP NUMBER 30194 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.633034441E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560888100E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124499351E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+01 0.58292E+02 Friction velocity uk : 0.10338E+01 0.58292E+02 Dimensionless distance yplus : 0.20548E-01 0.46232E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14432E-01 0.12598E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60122E+03 2 0.23838E-06 0.55316E+02 0.17956E+03 c Velocity[X] 0.11255E+01 c Velocity[Y] 0.10903E+02 c Velocity[Z] 0.43288E+02 c Pressure 0.76039E-01 8 0.91026E-08 0.33952E+07 0.48499E+02 c k 0.24763E+04 2 0.18982E-06 0.14692E+06 0.19311E+04 c omega 0.81517E+09 1 0.46292E-08 0.38936E+12 0.45689E+02 c TotEner 0.24226E+06 1 0.11164E-05 0.60952E+07 0.26876E+02 c temperature 0.00000E+00 0 0.00000E+00 0.13593E+02 0.29740E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9637e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.23 228.23 0.0018032 0.0011201 v Velocity[Y] -0.12995 701.9 250.55 81.06 v Velocity[Z] -19.167 368.18 25.28 1.9737 v ǁVelocityǁ 0.22734 701.9 260.34 83.799 v Pressure 49511 1.1024e+05 1.035e+05 1.0416e+05 v k 1.1773e-08 43019 912.87 355.37 v omega 154.5 9.6785e+09 1.846e+08 3.4145e+05 v TotEner 88760 6.295e+05 3.4162e+05 2.4856e+05 v temperature 58.942 533.94 397.85 337.21 v Density 0.3862 5.085 0.9489 1.0902 v TurbVisc 8.7664e-19 0.064107 0.010073 0.028648 v CourantNb 1.3178e-05 43.793 0.39423 0.007602 v FourierNb 4.5149e-05 203.95 1.8277 0.090687 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 59.059 533.94 402.52 421.85 v Boundary Density 0.38631 5.0775 0.99222 0.89917 v Yplus 0 46.232 2.4529 0.96069 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8442e-05 44.428 0.48443 0.010631 INSTANT 0.159182937E-01 TIME STEP NUMBER 30195 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.633656762E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560883144E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124493736E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+01 0.58296E+02 Friction velocity uk : 0.10338E+01 0.58296E+02 Dimensionless distance yplus : 0.20548E-01 0.46266E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14432E-01 0.12600E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60122E+03 2 0.23828E-06 0.55847E+02 0.18042E+03 c Velocity[X] 0.11241E+01 c Velocity[Y] 0.10951E+02 c Velocity[Z] 0.43772E+02 c Pressure 0.76043E-01 8 0.96872E-08 0.34386E+07 0.48808E+02 c k 0.24768E+04 2 0.19067E-06 0.14896E+06 0.19443E+04 c omega 0.81517E+09 1 0.45595E-08 0.40657E+12 0.46688E+02 c TotEner 0.24226E+06 1 0.11171E-05 0.61553E+07 0.27008E+02 c temperature 0.00000E+00 0 0.00000E+00 0.13756E+02 0.29918E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9632e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.25 228.25 0.0018051 0.0011229 v Velocity[Y] -0.12994 701.9 250.55 81.061 v Velocity[Z] -19.167 368.31 25.285 1.9739 v ǁVelocityǁ 0.2274 701.9 260.34 83.8 v Pressure 49495 1.1024e+05 1.035e+05 1.0416e+05 v k 1.1772e-08 43040 912.92 355.37 v omega 154.5 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 88674 6.295e+05 3.4162e+05 2.4856e+05 v temperature 58.825 533.94 397.85 337.21 v Density 0.3861 5.0926 0.94889 1.0902 v TurbVisc 8.7662e-19 0.064106 0.010073 0.028649 v CourantNb 1.3177e-05 43.801 0.3943 0.0076021 v FourierNb 4.5152e-05 203.9 1.8275 0.090688 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 58.942 533.94 402.52 421.85 v Boundary Density 0.3862 5.085 0.99232 0.89919 v Yplus 0 46.266 2.4531 0.9608 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8441e-05 44.435 0.4845 0.010631 INSTANT 0.159185568E-01 TIME STEP NUMBER 30196 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.634317295E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560878243E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124487510E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10338E+01 0.58299E+02 Friction velocity uk : 0.10338E+01 0.58299E+02 Dimensionless distance yplus : 0.20548E-01 0.46300E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14432E-01 0.12602E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60122E+03 2 0.23818E-06 0.56319E+02 0.18118E+03 c Velocity[X] 0.11230E+01 c Velocity[Y] 0.10930E+02 c Velocity[Z] 0.44266E+02 c Pressure 0.76047E-01 10 0.62892E-08 0.34831E+07 0.49123E+02 c k 0.24772E+04 2 0.19152E-06 0.15083E+06 0.19562E+04 c omega 0.81517E+09 1 0.46108E-08 0.39750E+12 0.46164E+02 c TotEner 0.24227E+06 1 0.11176E-05 0.61971E+07 0.27100E+02 c temperature 0.00000E+00 0 0.00000E+00 0.13917E+02 0.30092E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9628e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.28 228.28 0.001807 0.0011258 v Velocity[Y] -0.12994 701.9 250.55 81.062 v Velocity[Z] -19.166 368.43 25.291 1.9741 v ǁVelocityǁ 0.22746 701.9 260.35 83.801 v Pressure 49479 1.1024e+05 1.0349e+05 1.0416e+05 v k 1.1772e-08 43061 912.98 355.37 v omega 154.51 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 88588 6.295e+05 3.4163e+05 2.4856e+05 v temperature 58.707 533.94 397.85 337.21 v Density 0.38599 5.1003 0.94889 1.0902 v TurbVisc 8.7659e-19 0.064106 0.010073 0.028649 v CourantNb 1.3176e-05 43.809 0.39436 0.0076023 v FourierNb 4.5154e-05 203.85 1.8273 0.090689 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 58.825 533.94 402.51 421.85 v Boundary Density 0.3861 5.0926 0.99241 0.89921 v Yplus 0 46.3 2.4532 0.9609 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.844e-05 44.442 0.48457 0.010631 INSTANT 0.159188198E-01 TIME STEP NUMBER 30197 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.635015871E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560873408E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124480669E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58303E+02 Friction velocity uk : 0.10337E+01 0.58303E+02 Dimensionless distance yplus : 0.20548E-01 0.46335E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14432E-01 0.12604E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60122E+03 2 0.23808E-06 0.56799E+02 0.18195E+03 c Velocity[X] 0.11221E+01 c Velocity[Y] 0.10906E+02 c Velocity[Z] 0.44771E+02 c Pressure 0.76051E-01 8 0.92276E-08 0.35282E+07 0.49440E+02 c k 0.24777E+04 2 0.19237E-06 0.15273E+06 0.19683E+04 c omega 0.81517E+09 1 0.42408E-08 0.31574E+12 0.41144E+02 c TotEner 0.24227E+06 1 0.11182E-05 0.62403E+07 0.27194E+02 c temperature 0.00000E+00 0 0.00000E+00 0.14081E+02 0.30269E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9623e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.3 228.3 0.0018091 0.0011286 v Velocity[Y] -0.12994 701.9 250.55 81.062 v Velocity[Z] -19.166 368.56 25.296 1.9743 v ǁVelocityǁ 0.22752 701.9 260.35 83.802 v Pressure 49463 1.1024e+05 1.0349e+05 1.0416e+05 v k 1.1772e-08 43082 913.03 355.37 v omega 154.51 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 88501 6.295e+05 3.4163e+05 2.4856e+05 v temperature 58.588 533.94 397.85 337.22 v Density 0.38589 5.1081 0.94888 1.0902 v TurbVisc 8.7657e-19 0.064105 0.010073 0.028649 v CourantNb 1.3175e-05 43.816 0.39443 0.0076024 v FourierNb 4.5156e-05 203.81 1.8271 0.09069 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 58.707 533.94 402.5 421.85 v Boundary Density 0.38599 5.1003 0.99251 0.89923 v Yplus 0 46.335 2.4533 0.961 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8438e-05 44.448 0.48463 0.010631 INSTANT 0.159190828E-01 TIME STEP NUMBER 30198 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.635752282E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560868643E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124473208E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58306E+02 Friction velocity uk : 0.10337E+01 0.58306E+02 Dimensionless distance yplus : 0.20548E-01 0.46370E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14431E-01 0.12606E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60122E+03 2 0.23799E-06 0.57300E+02 0.18275E+03 c Velocity[X] 0.11216E+01 c Velocity[Y] 0.10890E+02 c Velocity[Z] 0.45288E+02 c Pressure 0.76055E-01 8 0.97163E-08 0.35741E+07 0.49761E+02 c k 0.24781E+04 2 0.19325E-06 0.15474E+06 0.19809E+04 c omega 0.81517E+09 1 0.42337E-08 0.37319E+12 0.44730E+02 c TotEner 0.24227E+06 1 0.11188E-05 0.62870E+07 0.27295E+02 c temperature 0.00000E+00 0 0.00000E+00 0.14249E+02 0.30449E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9619e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.33 228.33 0.0018111 0.0011314 v Velocity[Y] -0.12994 701.9 250.55 81.063 v Velocity[Z] -19.165 368.69 25.301 1.9745 v ǁVelocityǁ 0.22758 701.9 260.36 83.803 v Pressure 49447 1.1024e+05 1.0349e+05 1.0416e+05 v k 1.1771e-08 43103 913.08 355.37 v omega 154.52 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 88413 6.295e+05 3.4163e+05 2.4856e+05 v temperature 58.468 533.94 397.84 337.22 v Density 0.38578 5.116 0.94888 1.0902 v TurbVisc 8.7654e-19 0.064105 0.010073 0.028649 v CourantNb 1.3174e-05 43.824 0.39449 0.0076025 v FourierNb 4.5158e-05 203.76 1.8269 0.090691 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 58.588 533.94 402.49 421.85 v Boundary Density 0.38589 5.1081 0.99261 0.89925 v Yplus 0 46.37 2.4534 0.96111 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8437e-05 44.455 0.4847 0.010632 INSTANT 0.159193459E-01 TIME STEP NUMBER 30199 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.636526275E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560863945E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124465121E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58310E+02 Friction velocity uk : 0.10337E+01 0.58310E+02 Dimensionless distance yplus : 0.20548E-01 0.46405E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14431E-01 0.12607E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60123E+03 2 0.23789E-06 0.57829E+02 0.18358E+03 c Velocity[X] 0.11214E+01 c Velocity[Y] 0.10890E+02 c Velocity[Z] 0.45817E+02 c Pressure 0.76059E-01 10 0.68498E-08 0.36213E+07 0.50088E+02 c k 0.24786E+04 2 0.19419E-06 0.15685E+06 0.19942E+04 c omega 0.81517E+09 1 0.40250E-08 0.36071E+12 0.43976E+02 c TotEner 0.24227E+06 1 0.11194E-05 0.63400E+07 0.27410E+02 c temperature 0.00000E+00 0 0.00000E+00 0.14423E+02 0.30634E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9614e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.36 228.36 0.001813 0.0011342 v Velocity[Y] -0.12993 701.9 250.55 81.064 v Velocity[Z] -19.165 368.81 25.306 1.9748 v ǁVelocityǁ 0.22764 701.9 260.36 83.804 v Pressure 49430 1.1024e+05 1.0349e+05 1.0416e+05 v k 1.1771e-08 43124 913.14 355.37 v omega 154.52 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 88325 6.295e+05 3.4163e+05 2.4856e+05 v temperature 58.347 533.94 397.84 337.22 v Density 0.38568 5.124 0.94888 1.0902 v TurbVisc 8.7652e-19 0.064104 0.010074 0.028649 v CourantNb 1.3173e-05 43.832 0.39456 0.0076027 v FourierNb 4.5161e-05 203.71 1.8267 0.090692 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 58.468 533.94 402.48 421.85 v Boundary Density 0.38578 5.116 0.99272 0.89927 v Yplus 0 46.405 2.4536 0.96121 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8435e-05 44.462 0.48477 0.010632 INSTANT 0.159196089E-01 TIME STEP NUMBER 30200 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.637337561E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560859345E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124456405E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58314E+02 Friction velocity uk : 0.10337E+01 0.58314E+02 Dimensionless distance yplus : 0.20547E-01 0.46441E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14431E-01 0.12609E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60123E+03 2 0.23779E-06 0.58374E+02 0.18445E+03 c Velocity[X] 0.11215E+01 c Velocity[Y] 0.10895E+02 c Velocity[Z] 0.46358E+02 c Pressure 0.76063E-01 10 0.73919E-08 0.36691E+07 0.50418E+02 c k 0.24790E+04 2 0.19516E-06 0.15905E+06 0.20079E+04 c omega 0.81517E+09 1 0.41383E-08 0.34269E+12 0.42864E+02 c TotEner 0.24227E+06 1 0.11201E-05 0.63938E+07 0.27526E+02 c temperature 0.00000E+00 0 0.00000E+00 0.14599E+02 0.30821E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.961e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.38 228.38 0.0018148 0.001137 v Velocity[Y] -0.12993 701.9 250.55 81.065 v Velocity[Z] -19.164 368.94 25.311 1.975 v ǁVelocityǁ 0.2277 701.9 260.36 83.805 v Pressure 49414 1.1024e+05 1.0349e+05 1.0416e+05 v k 1.1771e-08 43146 913.19 355.37 v omega 154.53 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 88236 6.295e+05 3.4163e+05 2.4856e+05 v temperature 58.225 533.94 397.84 337.22 v Density 0.38557 5.132 0.94887 1.0902 v TurbVisc 8.765e-19 0.064104 0.010074 0.028649 v CourantNb 1.3172e-05 43.84 0.39462 0.0076028 v FourierNb 4.5163e-05 203.67 1.8265 0.090693 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 58.347 533.94 402.48 421.84 v Boundary Density 0.38568 5.124 0.99282 0.89929 v Yplus 0 46.441 2.4537 0.96132 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8433e-05 44.469 0.48483 0.010632 INSTANT 0.159198720E-01 TIME STEP NUMBER 30201 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.638185808E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560854840E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124447055E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58317E+02 Friction velocity uk : 0.10337E+01 0.58317E+02 Dimensionless distance yplus : 0.20547E-01 0.46477E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14431E-01 0.12611E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60123E+03 2 0.23770E-06 0.58930E+02 0.18532E+03 c Velocity[X] 0.11219E+01 c Velocity[Y] 0.10898E+02 c Velocity[Z] 0.46910E+02 c Pressure 0.76067E-01 10 0.71640E-08 0.37180E+07 0.50753E+02 c k 0.24795E+04 2 0.19617E-06 0.16124E+06 0.20214E+04 c omega 0.81517E+09 1 0.37675E-08 0.31103E+12 0.40835E+02 c TotEner 0.24227E+06 1 0.11209E-05 0.64479E+07 0.27642E+02 c temperature 0.00000E+00 0 0.00000E+00 0.14779E+02 0.31010E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9605e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.41 228.41 0.0018165 0.0011398 v Velocity[Y] -0.12993 701.9 250.55 81.066 v Velocity[Z] -19.164 369.07 25.317 1.9752 v ǁVelocityǁ 0.22775 701.9 260.37 83.806 v Pressure 49398 1.1024e+05 1.0349e+05 1.0416e+05 v k 1.1771e-08 43167 913.24 355.37 v omega 154.53 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 88146 6.295e+05 3.4163e+05 2.4856e+05 v temperature 58.102 533.94 397.84 337.22 v Density 0.38546 5.1402 0.94887 1.0902 v TurbVisc 8.7647e-19 0.064103 0.010074 0.02865 v CourantNb 1.317e-05 43.848 0.39469 0.007603 v FourierNb 4.5165e-05 203.62 1.8263 0.090694 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 58.225 533.94 402.47 421.84 v Boundary Density 0.38557 5.132 0.99292 0.89931 v Yplus 0 46.477 2.4538 0.96143 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8432e-05 44.476 0.4849 0.010632 INSTANT 0.159201350E-01 TIME STEP NUMBER 30202 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.639070642E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560850408E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124437064E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58321E+02 Friction velocity uk : 0.10337E+01 0.58321E+02 Dimensionless distance yplus : 0.20547E-01 0.46513E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14431E-01 0.12613E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60123E+03 2 0.23760E-06 0.59488E+02 0.18619E+03 c Velocity[X] 0.11226E+01 c Velocity[Y] 0.10890E+02 c Velocity[Z] 0.47475E+02 c Pressure 0.76071E-01 10 0.64382E-08 0.37679E+07 0.51092E+02 c k 0.24799E+04 2 0.19723E-06 0.16350E+06 0.20352E+04 c omega 0.81517E+09 1 0.39921E-08 0.30000E+12 0.40105E+02 c TotEner 0.24227E+06 1 0.11216E-05 0.65005E+07 0.27755E+02 c temperature 0.00000E+00 0 0.00000E+00 0.14962E+02 0.31202E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9601e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.43 228.43 0.0018178 0.0011426 v Velocity[Y] -0.12993 701.9 250.56 81.067 v Velocity[Z] -19.163 369.2 25.322 1.9754 v ǁVelocityǁ 0.22781 701.9 260.37 83.806 v Pressure 49382 1.1024e+05 1.0349e+05 1.0416e+05 v k 1.177e-08 43189 913.3 355.37 v omega 154.54 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 88055 6.295e+05 3.4163e+05 2.4856e+05 v temperature 57.977 533.94 397.84 337.22 v Density 0.38536 5.1484 0.94886 1.0902 v TurbVisc 8.7645e-19 0.064103 0.010074 0.02865 v CourantNb 1.3169e-05 43.856 0.39476 0.0076031 v FourierNb 4.5168e-05 203.57 1.8261 0.090695 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 58.102 533.94 402.46 421.84 v Boundary Density 0.38546 5.1402 0.99303 0.89933 v Yplus 0 46.513 2.4539 0.96153 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.843e-05 44.482 0.48497 0.010632 INSTANT 0.159203980E-01 TIME STEP NUMBER 30203 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.639991653E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560846060E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124426430E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58325E+02 Friction velocity uk : 0.10337E+01 0.58325E+02 Dimensionless distance yplus : 0.20547E-01 0.46550E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14431E-01 0.12615E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60123E+03 2 0.23751E-06 0.60053E+02 0.18708E+03 c Velocity[X] 0.11235E+01 c Velocity[Y] 0.10877E+02 c Velocity[Z] 0.48052E+02 c Pressure 0.76075E-01 10 0.65459E-08 0.38187E+07 0.51436E+02 c k 0.24804E+04 2 0.19831E-06 0.16579E+06 0.20492E+04 c omega 0.81517E+09 1 0.34705E-08 0.22510E+12 0.34739E+02 c TotEner 0.24228E+06 1 0.11224E-05 0.65531E+07 0.27867E+02 c temperature 0.00000E+00 0 0.00000E+00 0.15148E+02 0.31395E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9596e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.46 228.46 0.0018191 0.0011454 v Velocity[Y] -0.12992 701.9 250.56 81.068 v Velocity[Z] -19.163 369.32 25.327 1.9756 v ǁVelocityǁ 0.22787 701.9 260.38 83.807 v Pressure 49366 1.1024e+05 1.0349e+05 1.0416e+05 v k 1.177e-08 43211 913.36 355.37 v omega 154.54 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 87963 6.295e+05 3.4163e+05 2.4856e+05 v temperature 57.852 533.94 397.84 337.22 v Density 0.38525 5.1568 0.94886 1.0902 v TurbVisc 8.7643e-19 0.064102 0.010074 0.02865 v CourantNb 1.3168e-05 43.864 0.39482 0.0076032 v FourierNb 4.517e-05 203.53 1.8259 0.090696 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 57.977 533.94 402.45 421.84 v Boundary Density 0.38536 5.1484 0.99313 0.89936 v Yplus 0 46.55 2.4541 0.96164 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8428e-05 44.489 0.48503 0.010633 INSTANT 0.159206611E-01 TIME STEP NUMBER 30204 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.640948388E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560841793E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124415145E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58328E+02 Friction velocity uk : 0.10337E+01 0.58328E+02 Dimensionless distance yplus : 0.20547E-01 0.46587E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14431E-01 0.12617E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60124E+03 2 0.23741E-06 0.60649E+02 0.18800E+03 c Velocity[X] 0.11247E+01 c Velocity[Y] 0.10882E+02 c Velocity[Z] 0.48642E+02 c Pressure 0.76079E-01 10 0.71519E-08 0.38705E+07 0.51783E+02 c k 0.24809E+04 2 0.19943E-06 0.16820E+06 0.20638E+04 c omega 0.81517E+09 1 0.35602E-08 0.25185E+12 0.36746E+02 c TotEner 0.24228E+06 1 0.11232E-05 0.66110E+07 0.27990E+02 c temperature 0.00000E+00 0 0.00000E+00 0.15340E+02 0.31593E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9592e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.49 228.49 0.0018201 0.0011481 v Velocity[Y] -0.12992 701.9 250.56 81.069 v Velocity[Z] -19.162 369.45 25.333 1.9758 v ǁVelocityǁ 0.22792 701.9 260.38 83.808 v Pressure 49349 1.1024e+05 1.0348e+05 1.0416e+05 v k 1.177e-08 43233 913.41 355.37 v omega 154.55 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 87871 6.295e+05 3.4163e+05 2.4856e+05 v temperature 57.726 533.94 397.83 337.22 v Density 0.38515 5.1652 0.94886 1.0902 v TurbVisc 8.764e-19 0.064102 0.010074 0.02865 v CourantNb 1.3166e-05 43.872 0.39489 0.0076034 v FourierNb 4.5173e-05 203.48 1.8257 0.090697 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 57.852 533.94 402.44 421.84 v Boundary Density 0.38525 5.1568 0.99324 0.89938 v Yplus 0 46.587 2.4542 0.96176 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8426e-05 44.496 0.4851 0.010633 INSTANT 0.159209241E-01 TIME STEP NUMBER 30205 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.641940356E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560837586E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124403205E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58332E+02 Friction velocity uk : 0.10337E+01 0.58332E+02 Dimensionless distance yplus : 0.20547E-01 0.46625E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14431E-01 0.12619E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60124E+03 2 0.23732E-06 0.61255E+02 0.18894E+03 c Velocity[X] 0.11261E+01 c Velocity[Y] 0.10883E+02 c Velocity[Z] 0.49245E+02 c Pressure 0.76083E-01 8 0.99852E-08 0.39236E+07 0.52137E+02 c k 0.24814E+04 2 0.20061E-06 0.17068E+06 0.20787E+04 c omega 0.81517E+09 1 0.38328E-08 0.26413E+12 0.37631E+02 c TotEner 0.24228E+06 1 0.11241E-05 0.66702E+07 0.28115E+02 c temperature 0.00000E+00 0 0.00000E+00 0.15536E+02 0.31794E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9587e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.51 228.51 0.0018209 0.0011509 v Velocity[Y] -0.12992 701.9 250.56 81.07 v Velocity[Z] -19.162 369.58 25.338 1.976 v ǁVelocityǁ 0.22798 701.9 260.38 83.809 v Pressure 49333 1.1024e+05 1.0348e+05 1.0416e+05 v k 1.1769e-08 43255 913.47 355.37 v omega 154.55 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 87778 6.295e+05 3.4163e+05 2.4856e+05 v temperature 57.599 533.94 397.83 337.22 v Density 0.38504 5.1737 0.94885 1.0902 v TurbVisc 8.7638e-19 0.064102 0.010074 0.02865 v CourantNb 1.3165e-05 43.88 0.39495 0.0076035 v FourierNb 4.5175e-05 203.43 1.8255 0.090698 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 57.726 533.94 402.43 421.84 v Boundary Density 0.38515 5.1652 0.99335 0.8994 v Yplus 0 46.625 2.4544 0.96187 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8424e-05 44.503 0.48517 0.010633 INSTANT 0.159211872E-01 TIME STEP NUMBER 30206 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.642967029E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560833426E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124390604E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58335E+02 Friction velocity uk : 0.10337E+01 0.58335E+02 Dimensionless distance yplus : 0.20547E-01 0.46663E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14431E-01 0.12621E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60124E+03 2 0.23723E-06 0.61866E+02 0.18987E+03 c Velocity[X] 0.11277E+01 c Velocity[Y] 0.10877E+02 c Velocity[Z] 0.49861E+02 c Pressure 0.76087E-01 8 0.98909E-08 0.39776E+07 0.52495E+02 c k 0.24818E+04 2 0.20181E-06 0.17322E+06 0.20938E+04 c omega 0.81517E+09 1 0.42317E-08 0.38615E+12 0.45500E+02 c TotEner 0.24228E+06 1 0.11249E-05 0.67283E+07 0.28237E+02 c temperature 0.00000E+00 0 0.00000E+00 0.15735E+02 0.31997E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9583e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.54 228.54 0.0018217 0.0011536 v Velocity[Y] -0.12992 701.9 250.56 81.071 v Velocity[Z] -19.161 369.71 25.343 1.9762 v ǁVelocityǁ 0.22803 701.9 260.39 83.81 v Pressure 49317 1.1024e+05 1.0348e+05 1.0416e+05 v k 1.1769e-08 43277 913.53 355.37 v omega 154.56 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 87684 6.295e+05 3.4163e+05 2.4856e+05 v temperature 57.47 533.94 397.83 337.22 v Density 0.38494 5.1824 0.94885 1.0902 v TurbVisc 8.7635e-19 0.064101 0.010074 0.02865 v CourantNb 1.3163e-05 43.888 0.39502 0.0076037 v FourierNb 4.5178e-05 203.39 1.8253 0.090699 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 57.599 533.94 402.43 421.83 v Boundary Density 0.38504 5.1737 0.99346 0.89942 v Yplus 0 46.663 2.4545 0.96198 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8422e-05 44.509 0.48524 0.010633 INSTANT 0.159214502E-01 TIME STEP NUMBER 30207 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.644027837E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560829325E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124377336E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58339E+02 Friction velocity uk : 0.10337E+01 0.58339E+02 Dimensionless distance yplus : 0.20547E-01 0.46701E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14431E-01 0.12622E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60124E+03 2 0.23713E-06 0.62501E+02 0.19084E+03 c Velocity[X] 0.11295E+01 c Velocity[Y] 0.10881E+02 c Velocity[Z] 0.50490E+02 c Pressure 0.76091E-01 10 0.76189E-08 0.40327E+07 0.52858E+02 c k 0.24823E+04 2 0.20306E-06 0.17582E+06 0.21092E+04 c omega 0.81517E+09 1 0.41517E-08 0.35078E+12 0.43367E+02 c TotEner 0.24228E+06 1 0.11258E-05 0.67902E+07 0.28366E+02 c temperature 0.00000E+00 0 0.00000E+00 0.15939E+02 0.32204E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9578e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.57 228.57 0.0018222 0.0011564 v Velocity[Y] -0.12991 701.9 250.56 81.072 v Velocity[Z] -19.161 369.84 25.349 1.9764 v ǁVelocityǁ 0.22809 701.9 260.39 83.811 v Pressure 49301 1.1024e+05 1.0348e+05 1.0416e+05 v k 1.1769e-08 43299 913.59 355.37 v omega 154.56 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 87589 6.295e+05 3.4163e+05 2.4856e+05 v temperature 57.341 533.94 397.83 337.22 v Density 0.38483 5.1911 0.94884 1.0902 v TurbVisc 8.7633e-19 0.064101 0.010074 0.028651 v CourantNb 1.3162e-05 43.896 0.39509 0.0076038 v FourierNb 4.518e-05 203.34 1.8251 0.0907 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 57.47 533.94 402.42 421.83 v Boundary Density 0.38494 5.1824 0.99357 0.89945 v Yplus 0 46.701 2.4546 0.9621 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.842e-05 44.516 0.4853 0.010633 INSTANT 0.159217133E-01 TIME STEP NUMBER 30208 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.645122177E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560825285E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124363396E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58343E+02 Friction velocity uk : 0.10337E+01 0.58343E+02 Dimensionless distance yplus : 0.20546E-01 0.46740E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14431E-01 0.12624E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60124E+03 2 0.23704E-06 0.63144E+02 0.19182E+03 c Velocity[X] 0.11315E+01 c Velocity[Y] 0.10880E+02 c Velocity[Z] 0.51133E+02 c Pressure 0.76095E-01 10 0.73475E-08 0.40890E+07 0.53225E+02 c k 0.24828E+04 2 0.20435E-06 0.17848E+06 0.21248E+04 c omega 0.81517E+09 1 0.38776E-08 0.29118E+12 0.39511E+02 c TotEner 0.24228E+06 1 0.11268E-05 0.68521E+07 0.28495E+02 c temperature 0.00000E+00 0 0.00000E+00 0.16147E+02 0.32413E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9574e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.59 228.59 0.0018226 0.0011591 v Velocity[Y] -0.12991 701.9 250.56 81.073 v Velocity[Z] -19.16 369.97 25.354 1.9766 v ǁVelocityǁ 0.22814 701.9 260.4 83.812 v Pressure 49284 1.1024e+05 1.0348e+05 1.0416e+05 v k 1.1768e-08 43321 913.65 355.36 v omega 154.57 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 87493 6.295e+05 3.4163e+05 2.4856e+05 v temperature 57.21 533.94 397.83 337.22 v Density 0.38472 5.1999 0.94884 1.0902 v TurbVisc 8.7631e-19 0.0641 0.010074 0.028651 v CourantNb 1.316e-05 43.904 0.39515 0.007604 v FourierNb 4.5183e-05 203.29 1.8249 0.090701 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 57.341 533.94 402.41 421.83 v Boundary Density 0.38483 5.1911 0.99368 0.89947 v Yplus 0 46.74 2.4548 0.96221 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8418e-05 44.523 0.48537 0.010634 INSTANT 0.159219763E-01 TIME STEP NUMBER 30209 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.646249406E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560821294E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124348778E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58346E+02 Friction velocity uk : 0.10337E+01 0.58346E+02 Dimensionless distance yplus : 0.20546E-01 0.46780E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14430E-01 0.12626E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60125E+03 2 0.23695E-06 0.63802E+02 0.19282E+03 c Velocity[X] 0.11337E+01 c Velocity[Y] 0.10878E+02 c Velocity[Z] 0.51790E+02 c Pressure 0.76099E-01 10 0.73845E-08 0.41465E+07 0.53598E+02 c k 0.24833E+04 2 0.20567E-06 0.18120E+06 0.21407E+04 c omega 0.81518E+09 1 0.35631E-08 0.24378E+12 0.36152E+02 c TotEner 0.24228E+06 1 0.11278E-05 0.69151E+07 0.28626E+02 c temperature 0.00000E+00 0 0.00000E+00 0.16360E+02 0.32626E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9569e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.62 228.62 0.0018228 0.0011618 v Velocity[Y] -0.12991 701.9 250.56 81.074 v Velocity[Z] -19.16 370.1 25.359 1.9768 v ǁVelocityǁ 0.22819 701.9 260.4 83.813 v Pressure 49268 1.1024e+05 1.0348e+05 1.0416e+05 v k 1.1768e-08 43344 913.71 355.36 v omega 154.57 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 87397 6.295e+05 3.4163e+05 2.4856e+05 v temperature 57.078 533.94 397.82 337.22 v Density 0.38462 5.2089 0.94883 1.0902 v TurbVisc 8.7629e-19 0.0641 0.010074 0.028651 v CourantNb 1.3158e-05 43.912 0.39522 0.0076041 v FourierNb 4.5185e-05 203.25 1.8247 0.090703 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 57.21 533.94 402.4 421.83 v Boundary Density 0.38472 5.1999 0.99379 0.89949 v Yplus 0 46.78 2.4549 0.96233 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8415e-05 44.53 0.48544 0.010634 INSTANT 0.159222393E-01 TIME STEP NUMBER 30210 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.647408845E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560817350E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124333474E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58350E+02 Friction velocity uk : 0.10337E+01 0.58350E+02 Dimensionless distance yplus : 0.20546E-01 0.46819E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14430E-01 0.12628E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60125E+03 2 0.23686E-06 0.64475E+02 0.19383E+03 c Velocity[X] 0.11360E+01 c Velocity[Y] 0.10879E+02 c Velocity[Z] 0.52460E+02 c Pressure 0.76103E-01 10 0.74001E-08 0.42052E+07 0.53976E+02 c k 0.24838E+04 2 0.20704E-06 0.18399E+06 0.21569E+04 c omega 0.81518E+09 1 0.38903E-08 0.28989E+12 0.39423E+02 c TotEner 0.24229E+06 1 0.11288E-05 0.69801E+07 0.28760E+02 c temperature 0.00000E+00 0 0.00000E+00 0.16577E+02 0.32842E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9565e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.64 228.64 0.0018228 0.0011645 v Velocity[Y] -0.12991 701.9 250.56 81.075 v Velocity[Z] -19.159 370.23 25.365 1.977 v ǁVelocityǁ 0.22825 701.9 260.4 83.814 v Pressure 49252 1.1024e+05 1.0348e+05 1.0416e+05 v k 1.1768e-08 43366 913.77 355.36 v omega 154.58 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 87300 6.295e+05 3.4163e+05 2.4856e+05 v temperature 56.945 533.94 397.82 337.22 v Density 0.38451 5.218 0.94883 1.0902 v TurbVisc 8.7626e-19 0.064099 0.010075 0.028651 v CourantNb 1.3157e-05 43.92 0.39529 0.0076042 v FourierNb 4.5188e-05 203.2 1.8245 0.090704 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 57.078 533.94 402.39 421.83 v Boundary Density 0.38462 5.2089 0.99391 0.89952 v Yplus 0 46.819 2.4551 0.96245 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8413e-05 44.536 0.4855 0.010634 INSTANT 0.159225024E-01 TIME STEP NUMBER 30211 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.648599779E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560813463E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124317478E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58353E+02 Friction velocity uk : 0.10337E+01 0.58353E+02 Dimensionless distance yplus : 0.20546E-01 0.46860E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14430E-01 0.12631E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60125E+03 2 0.23677E-06 0.65171E+02 0.19487E+03 c Velocity[X] 0.11386E+01 c Velocity[Y] 0.10887E+02 c Velocity[Z] 0.53145E+02 c Pressure 0.76107E-01 10 0.74868E-08 0.42651E+07 0.54359E+02 c k 0.24843E+04 2 0.20844E-06 0.18686E+06 0.21733E+04 c omega 0.81518E+09 1 0.57571E-08 0.43499E+12 0.48292E+02 c TotEner 0.24229E+06 1 0.11299E-05 0.70485E+07 0.28901E+02 c temperature 0.00000E+00 0 0.00000E+00 0.16800E+02 0.33063E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.956e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.67 228.67 0.0018227 0.0011672 v Velocity[Y] -0.12991 701.9 250.56 81.076 v Velocity[Z] -19.159 370.36 25.37 1.9772 v ǁVelocityǁ 0.2283 701.9 260.41 83.815 v Pressure 49236 1.1024e+05 1.0348e+05 1.0416e+05 v k 1.1768e-08 43389 913.83 355.36 v omega 154.58 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 87201 6.295e+05 3.4163e+05 2.4856e+05 v temperature 56.811 533.94 397.82 337.22 v Density 0.3844 5.2271 0.94883 1.0902 v TurbVisc 8.7624e-19 0.064099 0.010075 0.028651 v CourantNb 1.3155e-05 43.928 0.39535 0.0076044 v FourierNb 4.5191e-05 203.15 1.8243 0.090705 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 56.945 533.94 402.38 421.83 v Boundary Density 0.38451 5.218 0.99402 0.89954 v Yplus 0 46.86 2.4552 0.96257 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.841e-05 44.543 0.48557 0.010634 INSTANT 0.159227654E-01 TIME STEP NUMBER 30212 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.649821460E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560809635E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124300784E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10337E+01 0.58357E+02 Friction velocity uk : 0.10337E+01 0.58357E+02 Dimensionless distance yplus : 0.20546E-01 0.46900E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14430E-01 0.12633E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60125E+03 2 0.23668E-06 0.65882E+02 0.19593E+03 c Velocity[X] 0.11414E+01 c Velocity[Y] 0.10896E+02 c Velocity[Z] 0.53845E+02 c Pressure 0.76111E-01 10 0.72550E-08 0.43265E+07 0.54749E+02 c k 0.24848E+04 2 0.20988E-06 0.18982E+06 0.21902E+04 c omega 0.81518E+09 1 0.55628E-08 0.42382E+12 0.47668E+02 c TotEner 0.24229E+06 1 0.11310E-05 0.71188E+07 0.29044E+02 c temperature 0.00000E+00 0 0.00000E+00 0.17029E+02 0.33286E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9556e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.7 228.7 0.0018225 0.0011699 v Velocity[Y] -0.1299 701.9 250.56 81.077 v Velocity[Z] -19.158 370.49 25.376 1.9774 v ǁVelocityǁ 0.22835 701.9 260.41 83.816 v Pressure 49219 1.1024e+05 1.0347e+05 1.0416e+05 v k 1.1767e-08 43412 913.89 355.36 v omega 154.59 9.6786e+09 1.846e+08 3.4145e+05 v TotEner 87102 6.295e+05 3.4163e+05 2.4856e+05 v temperature 56.676 533.94 397.82 337.22 v Density 0.3843 5.2364 0.94882 1.0902 v TurbVisc 8.7622e-19 0.064098 0.010075 0.028651 v CourantNb 1.3153e-05 43.936 0.39542 0.0076045 v FourierNb 4.5193e-05 203.11 1.8241 0.090706 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 56.811 533.94 402.37 421.82 v Boundary Density 0.3844 5.2271 0.99414 0.89957 v Yplus 0 46.9 2.4554 0.96269 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8408e-05 44.55 0.48564 0.010634 INSTANT 0.159230285E-01 TIME STEP NUMBER 30213 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.651073103E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560805870E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124283383E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58361E+02 Friction velocity uk : 0.10336E+01 0.58361E+02 Dimensionless distance yplus : 0.20546E-01 0.46942E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14430E-01 0.12635E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60126E+03 2 0.23659E-06 0.66598E+02 0.19699E+03 c Velocity[X] 0.11445E+01 c Velocity[Y] 0.10895E+02 c Velocity[Z] 0.54558E+02 c Pressure 0.76115E-01 10 0.69997E-08 0.43892E+07 0.55144E+02 c k 0.24854E+04 2 0.21140E-06 0.19287E+06 0.22074E+04 c omega 0.81518E+09 1 0.54689E-08 0.51704E+12 0.52650E+02 c TotEner 0.24229E+06 1 0.11322E-05 0.71882E+07 0.29186E+02 c temperature 0.00000E+00 0 0.00000E+00 0.17261E+02 0.33513E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9551e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.72 228.72 0.0018221 0.0011726 v Velocity[Y] -0.1299 701.9 250.56 81.078 v Velocity[Z] -19.158 370.62 25.381 1.9776 v ǁVelocityǁ 0.2284 701.9 260.42 83.817 v Pressure 49203 1.1024e+05 1.0347e+05 1.0416e+05 v k 1.1767e-08 43435 913.95 355.36 v omega 154.59 9.6786e+09 1.846e+08 3.4146e+05 v TotEner 87002 6.295e+05 3.4163e+05 2.4856e+05 v temperature 56.539 533.94 397.82 337.22 v Density 0.38419 5.2458 0.94882 1.0902 v TurbVisc 8.7619e-19 0.064098 0.010075 0.028652 v CourantNb 1.3151e-05 43.944 0.39549 0.0076047 v FourierNb 4.5196e-05 203.06 1.8239 0.090707 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 56.676 533.94 402.36 421.82 v Boundary Density 0.3843 5.2364 0.99426 0.89959 v Yplus 0 46.942 2.4556 0.96281 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8405e-05 44.557 0.48571 0.010635 INSTANT 0.159232915E-01 TIME STEP NUMBER 30214 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.652353889E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560802169E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124265268E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58364E+02 Friction velocity uk : 0.10336E+01 0.58364E+02 Dimensionless distance yplus : 0.20546E-01 0.46983E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14430E-01 0.12637E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60126E+03 2 0.23650E-06 0.67370E+02 0.19813E+03 c Velocity[X] 0.11478E+01 c Velocity[Y] 0.10935E+02 c Velocity[Z] 0.55288E+02 c Pressure 0.76119E-01 10 0.69138E-08 0.44533E+07 0.55546E+02 c k 0.24859E+04 2 0.21301E-06 0.19609E+06 0.22255E+04 c omega 0.81518E+09 1 0.48940E-08 0.43034E+12 0.48033E+02 c TotEner 0.24229E+06 1 0.11335E-05 0.72705E+07 0.29352E+02 c temperature 0.00000E+00 0 0.00000E+00 0.17503E+02 0.33747E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9547e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.75 228.75 0.0018218 0.0011753 v Velocity[Y] -0.1299 701.9 250.56 81.078 v Velocity[Z] -19.157 370.75 25.387 1.9778 v ǁVelocityǁ 0.22845 701.9 260.42 83.818 v Pressure 49187 1.1024e+05 1.0347e+05 1.0416e+05 v k 1.1767e-08 43458 914.01 355.36 v omega 154.6 9.6786e+09 1.846e+08 3.4146e+05 v TotEner 86901 6.295e+05 3.4163e+05 2.4856e+05 v temperature 56.401 533.94 397.82 337.22 v Density 0.38408 5.2553 0.94881 1.0902 v TurbVisc 8.7617e-19 0.064097 0.010075 0.028652 v CourantNb 1.3149e-05 43.952 0.39555 0.0076048 v FourierNb 4.5199e-05 203.02 1.8237 0.090708 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 56.539 533.94 402.35 421.82 v Boundary Density 0.38419 5.2458 0.99438 0.89962 v Yplus 0 46.983 2.4557 0.96294 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8402e-05 44.564 0.48577 0.010635 INSTANT 0.159235546E-01 TIME STEP NUMBER 30215 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.653662969E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560798541E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124246431E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58368E+02 Friction velocity uk : 0.10336E+01 0.58368E+02 Dimensionless distance yplus : 0.20546E-01 0.47025E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14430E-01 0.12639E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60126E+03 2 0.23641E-06 0.68112E+02 0.19921E+03 c Velocity[X] 0.11514E+01 c Velocity[Y] 0.10929E+02 c Velocity[Z] 0.56032E+02 c Pressure 0.76123E-01 8 0.94642E-08 0.45186E+07 0.55952E+02 c k 0.24864E+04 2 0.21458E-06 0.19921E+06 0.22428E+04 c omega 0.81518E+09 1 0.48452E-08 0.46596E+12 0.49981E+02 c TotEner 0.24229E+06 1 0.11347E-05 0.73399E+07 0.29492E+02 c temperature 0.00000E+00 0 0.00000E+00 0.17745E+02 0.33979E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9542e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.77 228.77 0.0018214 0.001178 v Velocity[Y] -0.1299 701.9 250.56 81.079 v Velocity[Z] -19.157 370.88 25.392 1.978 v ǁVelocityǁ 0.2285 701.9 260.42 83.819 v Pressure 49170 1.1024e+05 1.0347e+05 1.0416e+05 v k 1.1766e-08 43482 914.07 355.36 v omega 154.6 9.6786e+09 1.846e+08 3.4146e+05 v TotEner 86800 6.295e+05 3.4163e+05 2.4856e+05 v temperature 56.262 533.94 397.81 337.22 v Density 0.38398 5.265 0.94881 1.0902 v TurbVisc 8.7615e-19 0.064097 0.010075 0.028652 v CourantNb 1.3147e-05 43.96 0.39562 0.0076049 v FourierNb 4.5201e-05 202.97 1.8235 0.090709 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 56.401 533.94 402.34 421.82 v Boundary Density 0.38408 5.2553 0.9945 0.89964 v Yplus 0 47.025 2.4559 0.96306 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.84e-05 44.57 0.48584 0.010635 INSTANT 0.159238176E-01 TIME STEP NUMBER 30216 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.654999460E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560794997E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124226863E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58372E+02 Friction velocity uk : 0.10336E+01 0.58372E+02 Dimensionless distance yplus : 0.20545E-01 0.47068E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14430E-01 0.12641E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60126E+03 2 0.23633E-06 0.68885E+02 0.20034E+03 c Velocity[X] 0.11551E+01 c Velocity[Y] 0.10938E+02 c Velocity[Z] 0.56792E+02 c Pressure 0.76127E-01 8 0.97806E-08 0.45855E+07 0.56364E+02 c k 0.24869E+04 2 0.21621E-06 0.20247E+06 0.22608E+04 c omega 0.81518E+09 1 0.44004E-08 0.38805E+12 0.45612E+02 c TotEner 0.24229E+06 1 0.11360E-05 0.74167E+07 0.29646E+02 c temperature 0.00000E+00 0 0.00000E+00 0.17995E+02 0.34218E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9538e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.8 228.8 0.0018209 0.0011807 v Velocity[Y] -0.12989 701.9 250.56 81.08 v Velocity[Z] -19.157 371.01 25.398 1.9782 v ǁVelocityǁ 0.22855 701.9 260.43 83.819 v Pressure 49154 1.1024e+05 1.0347e+05 1.0416e+05 v k 1.1766e-08 43505 914.13 355.36 v omega 154.61 9.6786e+09 1.846e+08 3.4146e+05 v TotEner 86697 6.295e+05 3.4163e+05 2.4856e+05 v temperature 56.122 533.94 397.81 337.22 v Density 0.38387 5.2747 0.94881 1.0902 v TurbVisc 8.7612e-19 0.064097 0.010075 0.028652 v CourantNb 1.3145e-05 43.968 0.39569 0.0076051 v FourierNb 4.5204e-05 202.92 1.8233 0.09071 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 56.262 533.94 402.34 421.82 v Boundary Density 0.38398 5.265 0.99462 0.89967 v Yplus 0 47.068 2.456 0.96319 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8397e-05 44.577 0.48591 0.010635 INSTANT 0.159240807E-01 TIME STEP NUMBER 30217 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.656362447E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560791550E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124206556E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58375E+02 Friction velocity uk : 0.10336E+01 0.58375E+02 Dimensionless distance yplus : 0.20545E-01 0.47111E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14430E-01 0.12643E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60126E+03 2 0.23624E-06 0.69679E+02 0.20149E+03 c Velocity[X] 0.11592E+01 c Velocity[Y] 0.10953E+02 c Velocity[Z] 0.57568E+02 c Pressure 0.76131E-01 8 0.99699E-08 0.46536E+07 0.56781E+02 c k 0.24875E+04 2 0.21787E-06 0.20582E+06 0.22791E+04 c omega 0.81518E+09 1 0.43883E-08 0.41310E+12 0.47061E+02 c TotEner 0.24230E+06 1 0.11373E-05 0.74961E+07 0.29804E+02 c temperature 0.00000E+00 0 0.00000E+00 0.18250E+02 0.34459E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9533e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.83 228.83 0.0018202 0.0011833 v Velocity[Y] -0.12989 701.9 250.56 81.081 v Velocity[Z] -19.156 371.15 25.403 1.9784 v ǁVelocityǁ 0.2286 701.9 260.43 83.82 v Pressure 49137 1.1024e+05 1.0347e+05 1.0416e+05 v k 1.1766e-08 43529 914.2 355.36 v omega 154.61 9.6786e+09 1.846e+08 3.4146e+05 v TotEner 86593 6.295e+05 3.4163e+05 2.4856e+05 v temperature 55.98 533.94 397.81 337.22 v Density 0.38375 5.2846 0.9488 1.0902 v TurbVisc 8.761e-19 0.064096 0.010075 0.028652 v CourantNb 1.3143e-05 43.976 0.39575 0.0076052 v FourierNb 4.5207e-05 202.88 1.8231 0.090711 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 56.122 533.94 402.33 421.82 v Boundary Density 0.38387 5.2747 0.99475 0.89969 v Yplus 0 47.111 2.4562 0.96332 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8394e-05 44.584 0.48598 0.010635 INSTANT 0.159243437E-01 TIME STEP NUMBER 30218 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.657750986E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560788221E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124185500E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58379E+02 Friction velocity uk : 0.10336E+01 0.58379E+02 Dimensionless distance yplus : 0.20545E-01 0.47155E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14430E-01 0.12645E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60127E+03 2 0.23615E-06 0.70424E+02 0.20256E+03 c Velocity[X] 0.11635E+01 c Velocity[Y] 0.10902E+02 c Velocity[Z] 0.58358E+02 c Pressure 0.76135E-01 10 0.66945E-08 0.47237E+07 0.57207E+02 c k 0.24880E+04 2 0.21956E-06 0.20905E+06 0.22966E+04 c omega 0.81518E+09 1 0.45372E-08 0.45477E+12 0.49377E+02 c TotEner 0.24230E+06 1 0.11386E-05 0.75603E+07 0.29931E+02 c temperature 0.00000E+00 0 0.00000E+00 0.18506E+02 0.34700E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9528e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.85 228.85 0.0018192 0.0011859 v Velocity[Y] -0.12989 701.9 250.56 81.082 v Velocity[Z] -19.156 371.3 25.409 1.9787 v ǁVelocityǁ 0.22865 701.9 260.44 83.821 v Pressure 49121 1.1024e+05 1.0347e+05 1.0416e+05 v k 1.1765e-08 43552 914.26 355.36 v omega 154.62 9.6786e+09 1.8461e+08 3.4146e+05 v TotEner 86489 6.295e+05 3.4163e+05 2.4856e+05 v temperature 55.838 533.94 397.81 337.22 v Density 0.38363 5.2947 0.9488 1.0902 v TurbVisc 8.7607e-19 0.064096 0.010075 0.028652 v CourantNb 1.3141e-05 43.984 0.39582 0.0076054 v FourierNb 4.521e-05 202.83 1.8229 0.090712 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 55.98 533.94 402.32 421.81 v Boundary Density 0.38375 5.2846 0.99488 0.89972 v Yplus 0 47.155 2.4564 0.96345 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8391e-05 44.591 0.48604 0.010635 INSTANT 0.159246067E-01 TIME STEP NUMBER 30219 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.659164104E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560785011E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124163687E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58382E+02 Friction velocity uk : 0.10336E+01 0.58382E+02 Dimensionless distance yplus : 0.20545E-01 0.47199E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14430E-01 0.12648E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60127E+03 2 0.23606E-06 0.71241E+02 0.20373E+03 c Velocity[X] 0.11681E+01 c Velocity[Y] 0.10907E+02 c Velocity[Z] 0.59166E+02 c Pressure 0.76139E-01 10 0.69048E-08 0.47948E+07 0.57636E+02 c k 0.24886E+04 2 0.22132E-06 0.21251E+06 0.23152E+04 c omega 0.81518E+09 1 0.47316E-08 0.47778E+12 0.50611E+02 c TotEner 0.24230E+06 1 0.11400E-05 0.76418E+07 0.30092E+02 c temperature 0.00000E+00 0 0.00000E+00 0.18773E+02 0.34950E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9524e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.88 228.88 0.0018182 0.0011886 v Velocity[Y] -0.12989 701.9 250.56 81.083 v Velocity[Z] -19.155 371.45 25.415 1.9789 v ǁVelocityǁ 0.2287 701.9 260.44 83.822 v Pressure 49104 1.1024e+05 1.0346e+05 1.0416e+05 v k 1.1765e-08 43576 914.33 355.36 v omega 154.62 9.6786e+09 1.8461e+08 3.4146e+05 v TotEner 86383 6.295e+05 3.4163e+05 2.4856e+05 v temperature 55.693 533.94 397.81 337.22 v Density 0.38351 5.3048 0.94879 1.0902 v TurbVisc 8.7605e-19 0.064095 0.010075 0.028652 v CourantNb 1.3139e-05 43.992 0.39589 0.0076055 v FourierNb 4.5213e-05 202.79 1.8227 0.090713 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 55.838 533.94 402.31 421.81 v Boundary Density 0.38363 5.2947 0.995 0.89974 v Yplus 0 47.199 2.4566 0.96358 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8388e-05 44.598 0.48611 0.010636 INSTANT 0.159248698E-01 TIME STEP NUMBER 30220 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.660600797E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560781927E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124141106E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58386E+02 Friction velocity uk : 0.10336E+01 0.58386E+02 Dimensionless distance yplus : 0.20545E-01 0.47243E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14429E-01 0.12650E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60127E+03 2 0.23598E-06 0.72053E+02 0.20489E+03 c Velocity[X] 0.11731E+01 c Velocity[Y] 0.10889E+02 c Velocity[Z] 0.59991E+02 c Pressure 0.76144E-01 10 0.68075E-08 0.48677E+07 0.58073E+02 c k 0.24891E+04 2 0.22313E-06 0.21604E+06 0.23340E+04 c omega 0.81518E+09 1 0.47961E-08 0.43296E+12 0.48179E+02 c TotEner 0.24230E+06 1 0.11414E-05 0.77185E+07 0.30243E+02 c temperature 0.00000E+00 0 0.00000E+00 0.19044E+02 0.35201E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9519e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.91 228.91 0.0018171 0.0011912 v Velocity[Y] -0.12989 701.9 250.56 81.084 v Velocity[Z] -19.155 371.6 25.42 1.9791 v ǁVelocityǁ 0.22875 701.9 260.44 83.823 v Pressure 49088 1.1024e+05 1.0346e+05 1.0416e+05 v k 1.1765e-08 43600 914.39 355.36 v omega 154.63 9.6786e+09 1.8461e+08 3.4146e+05 v TotEner 86276 6.295e+05 3.4163e+05 2.4856e+05 v temperature 55.548 533.94 397.8 337.22 v Density 0.38339 5.3151 0.94879 1.0902 v TurbVisc 8.7603e-19 0.064095 0.010076 0.028653 v CourantNb 1.3136e-05 44 0.39595 0.0076057 v FourierNb 4.5216e-05 202.74 1.8225 0.090714 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 55.693 533.94 402.3 421.81 v Boundary Density 0.38351 5.3048 0.99513 0.89977 v Yplus 0 47.243 2.4567 0.96371 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8385e-05 44.604 0.48618 0.010636 INSTANT 0.159251328E-01 TIME STEP NUMBER 30221 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.662060037E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560778953E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124117747E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58390E+02 Friction velocity uk : 0.10336E+01 0.58390E+02 Dimensionless distance yplus : 0.20545E-01 0.47289E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14429E-01 0.12652E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60127E+03 2 0.23589E-06 0.72888E+02 0.20607E+03 c Velocity[X] 0.11784E+01 c Velocity[Y] 0.10877E+02 c Velocity[Z] 0.60832E+02 c Pressure 0.76148E-01 10 0.67448E-08 0.49423E+07 0.58516E+02 c k 0.24897E+04 2 0.22499E-06 0.21963E+06 0.23530E+04 c omega 0.81518E+09 1 0.41488E-08 0.31041E+12 0.40794E+02 c TotEner 0.24230E+06 1 0.11429E-05 0.77991E+07 0.30400E+02 c temperature 0.00000E+00 0 0.00000E+00 0.19321E+02 0.35456E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9515e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.93 228.93 0.0018159 0.0011938 v Velocity[Y] -0.12988 701.9 250.57 81.085 v Velocity[Z] -19.154 371.76 25.426 1.9793 v ǁVelocityǁ 0.22879 701.9 260.45 83.824 v Pressure 49071 1.1024e+05 1.0346e+05 1.0416e+05 v k 1.1764e-08 43625 914.46 355.36 v omega 154.63 9.6786e+09 1.8461e+08 3.4146e+05 v TotEner 86168 6.295e+05 3.4163e+05 2.4857e+05 v temperature 55.401 533.94 397.8 337.22 v Density 0.38328 5.3255 0.94879 1.0902 v TurbVisc 8.7601e-19 0.064094 0.010076 0.028653 v CourantNb 1.3134e-05 44.008 0.39602 0.0076058 v FourierNb 4.5219e-05 202.7 1.8223 0.090715 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 55.548 533.94 402.29 421.81 v Boundary Density 0.38339 5.3151 0.99526 0.8998 v Yplus 0 47.289 2.4569 0.96384 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8382e-05 44.611 0.48625 0.010636 INSTANT 0.159253959E-01 TIME STEP NUMBER 30222 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.663540765E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560776103E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124093599E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58393E+02 Friction velocity uk : 0.10336E+01 0.58393E+02 Dimensionless distance yplus : 0.20545E-01 0.47334E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14429E-01 0.12655E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60127E+03 2 0.23581E-06 0.73748E+02 0.20728E+03 c Velocity[X] 0.11841E+01 c Velocity[Y] 0.10873E+02 c Velocity[Z] 0.61691E+02 c Pressure 0.76152E-01 10 0.70353E-08 0.50185E+07 0.58966E+02 c k 0.24902E+04 2 0.22691E-06 0.22337E+06 0.23726E+04 c omega 0.81518E+09 1 0.34792E-08 0.22786E+12 0.34951E+02 c TotEner 0.24230E+06 1 0.11445E-05 0.78832E+07 0.30564E+02 c temperature 0.00000E+00 0 0.00000E+00 0.19606E+02 0.35716E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.951e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.96 228.96 0.0018143 0.0011964 v Velocity[Y] -0.12988 701.9 250.57 81.086 v Velocity[Z] -19.154 371.91 25.431 1.9795 v ǁVelocityǁ 0.22884 701.9 260.45 83.825 v Pressure 49055 1.1024e+05 1.0346e+05 1.0416e+05 v k 1.1764e-08 43649 914.53 355.36 v omega 154.64 9.6786e+09 1.8461e+08 3.4146e+05 v TotEner 86060 6.295e+05 3.4163e+05 2.4857e+05 v temperature 55.253 533.94 397.8 337.22 v Density 0.38316 5.3361 0.94878 1.0901 v TurbVisc 8.7599e-19 0.064094 0.010076 0.028653 v CourantNb 1.3132e-05 44.016 0.39609 0.0076059 v FourierNb 4.5222e-05 202.65 1.8221 0.090716 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 55.401 533.94 402.28 421.81 v Boundary Density 0.38328 5.3255 0.99539 0.89983 v Yplus 0 47.334 2.4571 0.96398 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8379e-05 44.618 0.48632 0.010636 INSTANT 0.159256589E-01 TIME STEP NUMBER 30223 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.665041900E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560773378E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124068650E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58397E+02 Friction velocity uk : 0.10336E+01 0.58397E+02 Dimensionless distance yplus : 0.20545E-01 0.47381E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14429E-01 0.12657E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60128E+03 2 0.23572E-06 0.74635E+02 0.20852E+03 c Velocity[X] 0.11901E+01 c Velocity[Y] 0.10877E+02 c Velocity[Z] 0.62567E+02 c Pressure 0.76156E-01 10 0.73603E-08 0.50967E+07 0.59423E+02 c k 0.24908E+04 2 0.22889E-06 0.22723E+06 0.23926E+04 c omega 0.81518E+09 1 0.33582E-08 0.22146E+12 0.34457E+02 c TotEner 0.24230E+06 1 0.11462E-05 0.79720E+07 0.30735E+02 c temperature 0.00000E+00 0 0.00000E+00 0.19898E+02 0.35981E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9506e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -228.98 228.98 0.0018126 0.0011989 v Velocity[Y] -0.12988 701.9 250.57 81.087 v Velocity[Z] -19.153 372.06 25.437 1.9797 v ǁVelocityǁ 0.22889 701.9 260.46 83.826 v Pressure 49038 1.1024e+05 1.0346e+05 1.0416e+05 v k 1.1764e-08 43674 914.6 355.36 v omega 154.64 9.6786e+09 1.8461e+08 3.4146e+05 v TotEner 85950 6.295e+05 3.4163e+05 2.4857e+05 v temperature 55.103 533.94 397.8 337.22 v Density 0.38304 5.3468 0.94878 1.0901 v TurbVisc 8.7597e-19 0.064093 0.010076 0.028653 v CourantNb 1.3129e-05 44.024 0.39616 0.0076061 v FourierNb 4.5225e-05 202.6 1.8219 0.090717 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 55.253 533.94 402.27 421.8 v Boundary Density 0.38316 5.3361 0.99553 0.89985 v Yplus 0 47.381 2.4573 0.96412 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8376e-05 44.625 0.48638 0.010636 INSTANT 0.159259220E-01 TIME STEP NUMBER 30224 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.666562334E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560770765E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124042889E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58401E+02 Friction velocity uk : 0.10336E+01 0.58401E+02 Dimensionless distance yplus : 0.20544E-01 0.47428E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14429E-01 0.12659E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60128E+03 2 0.23564E-06 0.75538E+02 0.20977E+03 c Velocity[X] 0.11966E+01 c Velocity[Y] 0.10879E+02 c Velocity[Z] 0.63462E+02 c Pressure 0.76160E-01 10 0.76927E-08 0.51768E+07 0.59888E+02 c k 0.24914E+04 2 0.23092E-06 0.23117E+06 0.24129E+04 c omega 0.81518E+09 1 0.38719E-08 0.25381E+12 0.36888E+02 c TotEner 0.24231E+06 1 0.11479E-05 0.80624E+07 0.30909E+02 c temperature 0.00000E+00 0 0.00000E+00 0.20197E+02 0.36251E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9501e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.01 229.01 0.0018107 0.0012015 v Velocity[Y] -0.12988 701.9 250.57 81.088 v Velocity[Z] -19.153 372.22 25.443 1.9799 v ǁVelocityǁ 0.22893 701.9 260.46 83.827 v Pressure 49022 1.1024e+05 1.0346e+05 1.0416e+05 v k 1.1764e-08 43698 914.66 355.36 v omega 154.65 9.6786e+09 1.8461e+08 3.4146e+05 v TotEner 85839 6.295e+05 3.4163e+05 2.4857e+05 v temperature 54.952 533.94 397.8 337.22 v Density 0.38292 5.3576 0.94878 1.0901 v TurbVisc 8.7594e-19 0.064093 0.010076 0.028653 v CourantNb 1.3127e-05 44.032 0.39622 0.0076062 v FourierNb 4.5228e-05 202.56 1.8217 0.090718 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 55.103 533.94 402.26 421.8 v Boundary Density 0.38304 5.3468 0.99566 0.89988 v Yplus 0 47.428 2.4575 0.96426 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8373e-05 44.632 0.48645 0.010637 INSTANT 0.159261850E-01 TIME STEP NUMBER 30225 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.668100936E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560768259E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.124016304E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58404E+02 Friction velocity uk : 0.10336E+01 0.58404E+02 Dimensionless distance yplus : 0.20544E-01 0.47475E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14429E-01 0.12662E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60128E+03 2 0.23556E-06 0.76458E+02 0.21105E+03 c Velocity[X] 0.12034E+01 c Velocity[Y] 0.10880E+02 c Velocity[Z] 0.64375E+02 c Pressure 0.76164E-01 10 0.77439E-08 0.52586E+07 0.60359E+02 c k 0.24920E+04 2 0.23300E-06 0.23520E+06 0.24335E+04 c omega 0.81518E+09 1 0.35993E-08 0.29662E+12 0.39878E+02 c TotEner 0.24231E+06 1 0.11496E-05 0.81541E+07 0.31084E+02 c temperature 0.00000E+00 0 0.00000E+00 0.20502E+02 0.36524E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9497e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.04 229.04 0.0018088 0.001204 v Velocity[Y] -0.12988 701.9 250.57 81.089 v Velocity[Z] -19.152 372.37 25.449 1.9801 v ǁVelocityǁ 0.22898 701.9 260.47 83.828 v Pressure 49005 1.1024e+05 1.0346e+05 1.0416e+05 v k 1.1763e-08 43723 914.73 355.36 v omega 154.65 9.6786e+09 1.8461e+08 3.4146e+05 v TotEner 85727 6.295e+05 3.4163e+05 2.4857e+05 v temperature 54.799 533.94 397.79 337.22 v Density 0.3828 5.3686 0.94877 1.0901 v TurbVisc 8.7592e-19 0.064093 0.010076 0.028653 v CourantNb 1.3125e-05 44.04 0.39629 0.0076064 v FourierNb 4.5231e-05 202.51 1.8215 0.090719 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 54.952 533.94 402.25 421.8 v Boundary Density 0.38292 5.3576 0.9958 0.89991 v Yplus 0 47.475 2.4577 0.9644 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.837e-05 44.639 0.48652 0.010637 INSTANT 0.159264481E-01 TIME STEP NUMBER 30226 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.669656553E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560765853E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123988882E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58408E+02 Friction velocity uk : 0.10336E+01 0.58408E+02 Dimensionless distance yplus : 0.20544E-01 0.47523E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14429E-01 0.12664E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60128E+03 2 0.23547E-06 0.77390E+02 0.21233E+03 c Velocity[X] 0.12107E+01 c Velocity[Y] 0.10873E+02 c Velocity[Z] 0.65307E+02 c Pressure 0.76168E-01 10 0.78775E-08 0.53424E+07 0.60839E+02 c k 0.24925E+04 2 0.23514E-06 0.23933E+06 0.24544E+04 c omega 0.81518E+09 1 0.39821E-08 0.34456E+12 0.42980E+02 c TotEner 0.24231E+06 1 0.11514E-05 0.82461E+07 0.31259E+02 c temperature 0.00000E+00 0 0.00000E+00 0.20814E+02 0.36800E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9492e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.06 229.06 0.0018067 0.0012066 v Velocity[Y] -0.12987 701.9 250.57 81.09 v Velocity[Z] -19.152 372.53 25.454 1.9803 v ǁVelocityǁ 0.22902 701.9 260.47 83.829 v Pressure 48989 1.1024e+05 1.0345e+05 1.0416e+05 v k 1.1763e-08 43748 914.81 355.36 v omega 154.66 9.6786e+09 1.8461e+08 3.4146e+05 v TotEner 85614 6.295e+05 3.4163e+05 2.4857e+05 v temperature 54.645 533.94 397.79 337.23 v Density 0.38268 5.3797 0.94877 1.0901 v TurbVisc 8.759e-19 0.064092 0.010076 0.028654 v CourantNb 1.3122e-05 44.049 0.39636 0.0076065 v FourierNb 4.5234e-05 202.47 1.8213 0.09072 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 54.799 533.94 402.24 421.8 v Boundary Density 0.3828 5.3686 0.99594 0.89994 v Yplus 0 47.523 2.4579 0.96454 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8366e-05 44.646 0.48659 0.010637 INSTANT 0.159267111E-01 TIME STEP NUMBER 30227 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.671228011E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560763548E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123960610E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58412E+02 Friction velocity uk : 0.10336E+01 0.58412E+02 Dimensionless distance yplus : 0.20544E-01 0.47572E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14429E-01 0.12666E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60129E+03 2 0.23539E-06 0.78335E+02 0.21362E+03 c Velocity[X] 0.12184E+01 c Velocity[Y] 0.10860E+02 c Velocity[Z] 0.66257E+02 c Pressure 0.76172E-01 10 0.79570E-08 0.54283E+07 0.61326E+02 c k 0.24931E+04 2 0.23734E-06 0.24355E+06 0.24756E+04 c omega 0.81518E+09 1 0.34785E-08 0.26107E+12 0.37412E+02 c TotEner 0.24231E+06 1 0.11532E-05 0.83395E+07 0.31435E+02 c temperature 0.00000E+00 0 0.00000E+00 0.21133E+02 0.37081E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9488e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.09 229.09 0.0018046 0.0012091 v Velocity[Y] -0.12987 701.9 250.57 81.091 v Velocity[Z] -19.151 372.68 25.46 1.9805 v ǁVelocityǁ 0.22907 701.9 260.47 83.83 v Pressure 48972 1.1024e+05 1.0345e+05 1.0416e+05 v k 1.1763e-08 43773 914.88 355.36 v omega 154.66 9.6786e+09 1.8461e+08 3.4146e+05 v TotEner 85500 6.295e+05 3.4163e+05 2.4857e+05 v temperature 54.489 533.94 397.79 337.23 v Density 0.38256 5.391 0.94876 1.0901 v TurbVisc 8.7588e-19 0.064092 0.010076 0.028654 v CourantNb 1.312e-05 44.057 0.39643 0.0076067 v FourierNb 4.5237e-05 202.42 1.8211 0.090721 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 54.645 533.94 402.23 421.8 v Boundary Density 0.38268 5.3797 0.99608 0.89997 v Yplus 0 47.572 2.4581 0.96468 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8363e-05 44.652 0.48666 0.010637 INSTANT 0.159269742E-01 TIME STEP NUMBER 30228 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.672814114E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560761342E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123931473E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58415E+02 Friction velocity uk : 0.10336E+01 0.58415E+02 Dimensionless distance yplus : 0.20544E-01 0.47621E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14429E-01 0.12669E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60129E+03 2 0.23531E-06 0.79322E+02 0.21496E+03 c Velocity[X] 0.12265E+01 c Velocity[Y] 0.10868E+02 c Velocity[Z] 0.67228E+02 c Pressure 0.76176E-01 10 0.91100E-08 0.55159E+07 0.61819E+02 c k 0.24937E+04 2 0.23961E-06 0.24795E+06 0.24975E+04 c omega 0.81518E+09 1 0.35005E-08 0.27606E+12 0.38471E+02 c TotEner 0.24231E+06 1 0.11552E-05 0.84394E+07 0.31623E+02 c temperature 0.00000E+00 0 0.00000E+00 0.21461E+02 0.37368E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9483e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.12 229.12 0.0018024 0.0012117 v Velocity[Y] -0.12987 701.9 250.57 81.092 v Velocity[Z] -19.151 372.84 25.466 1.9808 v ǁVelocityǁ 0.22911 701.9 260.48 83.831 v Pressure 48955 1.1024e+05 1.0345e+05 1.0416e+05 v k 1.1762e-08 43799 914.95 355.36 v omega 154.67 9.6786e+09 1.8461e+08 3.4146e+05 v TotEner 85385 6.295e+05 3.4164e+05 2.4857e+05 v temperature 54.332 533.94 397.79 337.23 v Density 0.38244 5.4025 0.94876 1.0901 v TurbVisc 8.7586e-19 0.064091 0.010076 0.028654 v CourantNb 1.3117e-05 44.065 0.39649 0.0076068 v FourierNb 4.524e-05 202.38 1.8209 0.090722 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 54.489 533.94 402.22 421.79 v Boundary Density 0.38256 5.391 0.99622 0.9 v Yplus 0 47.621 2.4583 0.96483 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.836e-05 44.659 0.48673 0.010637 INSTANT 0.159272372E-01 TIME STEP NUMBER 30229 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.674413648E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560759237E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123901457E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10336E+01 0.58419E+02 Friction velocity uk : 0.10336E+01 0.58419E+02 Dimensionless distance yplus : 0.20544E-01 0.47671E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14429E-01 0.12671E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60129E+03 2 0.23523E-06 0.80335E+02 0.21632E+03 c Velocity[X] 0.12350E+01 c Velocity[Y] 0.10882E+02 c Velocity[Z] 0.68218E+02 c Pressure 0.76180E-01 10 0.78624E-08 0.56059E+07 0.62321E+02 c k 0.24943E+04 2 0.24195E-06 0.25246E+06 0.25197E+04 c omega 0.81518E+09 1 0.35720E-08 0.26835E+12 0.37930E+02 c TotEner 0.24231E+06 1 0.11572E-05 0.85426E+07 0.31816E+02 c temperature 0.00000E+00 0 0.00000E+00 0.21797E+02 0.37659E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9479e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.14 229.14 0.0018001 0.0012142 v Velocity[Y] -0.12987 701.9 250.57 81.093 v Velocity[Z] -19.15 373 25.472 1.981 v ǁVelocityǁ 0.22916 701.9 260.48 83.832 v Pressure 48938 1.1024e+05 1.0345e+05 1.0416e+05 v k 1.1762e-08 43824 915.02 355.36 v omega 154.67 9.6786e+09 1.8461e+08 3.4146e+05 v TotEner 85268 6.295e+05 3.4164e+05 2.4857e+05 v temperature 54.174 533.94 397.79 337.23 v Density 0.38232 5.4141 0.94876 1.0901 v TurbVisc 8.7584e-19 0.064091 0.010077 0.028654 v CourantNb 1.3115e-05 44.073 0.39656 0.007607 v FourierNb 4.5243e-05 202.33 1.8207 0.090723 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 54.332 533.94 402.21 421.79 v Boundary Density 0.38244 5.4025 0.99637 0.90003 v Yplus 0 47.671 2.4585 0.96497 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8356e-05 44.666 0.48679 0.010638 INSTANT 0.159275003E-01 TIME STEP NUMBER 30230 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.676025382E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560757234E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123870548E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58423E+02 Friction velocity uk : 0.10335E+01 0.58423E+02 Dimensionless distance yplus : 0.20544E-01 0.47721E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14429E-01 0.12674E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60129E+03 2 0.23515E-06 0.81353E+02 0.21769E+03 c Velocity[X] 0.12441E+01 c Velocity[Y] 0.10880E+02 c Velocity[Z] 0.69229E+02 c Pressure 0.76184E-01 10 0.75794E-08 0.56981E+07 0.62832E+02 c k 0.24950E+04 2 0.24434E-06 0.25702E+06 0.25419E+04 c omega 0.81518E+09 1 0.40659E-08 0.34321E+12 0.42895E+02 c TotEner 0.24231E+06 1 0.11593E-05 0.86444E+07 0.32005E+02 c temperature 0.00000E+00 0 0.00000E+00 0.22139E+02 0.37954E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9474e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.17 229.17 0.0017975 0.0012167 v Velocity[Y] -0.12987 701.9 250.57 81.094 v Velocity[Z] -19.15 373.15 25.477 1.9812 v ǁVelocityǁ 0.2292 701.9 260.49 83.833 v Pressure 48922 1.1024e+05 1.0345e+05 1.0416e+05 v k 1.1762e-08 43850 915.09 355.36 v omega 154.68 9.6786e+09 1.8461e+08 3.4146e+05 v TotEner 85151 6.295e+05 3.4164e+05 2.4857e+05 v temperature 54.014 533.94 397.78 337.23 v Density 0.3822 5.4258 0.94875 1.0901 v TurbVisc 8.7581e-19 0.064091 0.010077 0.028654 v CourantNb 1.3112e-05 44.081 0.39663 0.0076071 v FourierNb 4.5246e-05 202.29 1.8205 0.090724 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 54.174 533.94 402.2 421.79 v Boundary Density 0.38232 5.4141 0.99651 0.90006 v Yplus 0 47.721 2.4587 0.96512 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8353e-05 44.673 0.48686 0.010638 INSTANT 0.159277633E-01 TIME STEP NUMBER 30231 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.677648066E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560755344E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123838729E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58426E+02 Friction velocity uk : 0.10335E+01 0.58426E+02 Dimensionless distance yplus : 0.20544E-01 0.47773E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14429E-01 0.12676E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60129E+03 2 0.23507E-06 0.82393E+02 0.21907E+03 c Velocity[X] 0.12536E+01 c Velocity[Y] 0.10879E+02 c Velocity[Z] 0.70260E+02 c Pressure 0.76188E-01 10 0.79693E-08 0.57925E+07 0.63350E+02 c k 0.24956E+04 2 0.24679E-06 0.26170E+06 0.25646E+04 c omega 0.81518E+09 1 0.40279E-08 0.31839E+12 0.41315E+02 c TotEner 0.24232E+06 1 0.11614E-05 0.87491E+07 0.32198E+02 c temperature 0.00000E+00 0 0.00000E+00 0.22490E+02 0.38253E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.947e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.2 229.2 0.0017948 0.0012192 v Velocity[Y] -0.12986 701.9 250.57 81.095 v Velocity[Z] -19.149 373.31 25.483 1.9814 v ǁVelocityǁ 0.22924 701.9 260.49 83.833 v Pressure 48905 1.1024e+05 1.0345e+05 1.0416e+05 v k 1.1762e-08 43876 915.17 355.36 v omega 154.68 9.6786e+09 1.8461e+08 3.4146e+05 v TotEner 85032 6.295e+05 3.4164e+05 2.4857e+05 v temperature 53.852 533.94 397.78 337.23 v Density 0.38208 5.4378 0.94875 1.0901 v TurbVisc 8.7579e-19 0.06409 0.010077 0.028654 v CourantNb 1.3109e-05 44.089 0.3967 0.0076072 v FourierNb 4.5249e-05 202.24 1.8204 0.090725 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 54.014 533.94 402.18 421.79 v Boundary Density 0.3822 5.4258 0.99666 0.90009 v Yplus 0 47.773 2.4589 0.96527 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8349e-05 44.68 0.48693 0.010638 INSTANT 0.159280264E-01 TIME STEP NUMBER 30232 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.679280435E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560753573E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123805984E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58430E+02 Friction velocity uk : 0.10335E+01 0.58430E+02 Dimensionless distance yplus : 0.20544E-01 0.47824E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14428E-01 0.12679E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60130E+03 2 0.23499E-06 0.83453E+02 0.22047E+03 c Velocity[X] 0.12635E+01 c Velocity[Y] 0.10877E+02 c Velocity[Z] 0.71313E+02 c Pressure 0.76192E-01 10 0.76454E-08 0.58893E+07 0.63877E+02 c k 0.24962E+04 2 0.24930E-06 0.26650E+06 0.25876E+04 c omega 0.81518E+09 1 0.44535E-08 0.33565E+12 0.42420E+02 c TotEner 0.24232E+06 1 0.11636E-05 0.88561E+07 0.32394E+02 c temperature 0.00000E+00 0 0.00000E+00 0.22849E+02 0.38557E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9465e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.22 229.22 0.0017919 0.0012217 v Velocity[Y] -0.12986 701.9 250.57 81.095 v Velocity[Z] -19.149 373.47 25.489 1.9816 v ǁVelocityǁ 0.22929 701.9 260.5 83.834 v Pressure 48888 1.1024e+05 1.0345e+05 1.0416e+05 v k 1.1761e-08 43902 915.24 355.36 v omega 154.69 9.6786e+09 1.8461e+08 3.4147e+05 v TotEner 84912 6.295e+05 3.4164e+05 2.4857e+05 v temperature 53.688 533.94 397.78 337.23 v Density 0.38196 5.4499 0.94874 1.0901 v TurbVisc 8.7577e-19 0.06409 0.010077 0.028655 v CourantNb 1.3107e-05 44.097 0.39677 0.0076074 v FourierNb 4.5253e-05 202.2 1.8202 0.090726 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 53.852 533.94 402.17 421.79 v Boundary Density 0.38208 5.4378 0.99681 0.90012 v Yplus 0 47.824 2.4591 0.96542 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8346e-05 44.687 0.487 0.010638 INSTANT 0.159282895E-01 TIME STEP NUMBER 30233 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.680921210E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560751929E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123772296E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58434E+02 Friction velocity uk : 0.10335E+01 0.58434E+02 Dimensionless distance yplus : 0.20543E-01 0.47877E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14428E-01 0.12682E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60130E+03 2 0.23491E-06 0.84530E+02 0.22189E+03 c Velocity[X] 0.12741E+01 c Velocity[Y] 0.10870E+02 c Velocity[Z] 0.72387E+02 c Pressure 0.76196E-01 10 0.76923E-08 0.59884E+07 0.64413E+02 c k 0.24968E+04 2 0.25188E-06 0.27140E+06 0.26108E+04 c omega 0.81518E+09 1 0.46744E-08 0.32083E+12 0.41473E+02 c TotEner 0.24232E+06 1 0.11658E-05 0.89646E+07 0.32592E+02 c temperature 0.00000E+00 0 0.00000E+00 0.23217E+02 0.38866E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9461e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.25 229.25 0.0017888 0.0012241 v Velocity[Y] -0.12986 701.9 250.57 81.096 v Velocity[Z] -19.148 373.63 25.495 1.9818 v ǁVelocityǁ 0.22933 701.9 260.5 83.835 v Pressure 48871 1.1024e+05 1.0344e+05 1.0416e+05 v k 1.1761e-08 43929 915.32 355.36 v omega 154.69 9.6786e+09 1.8461e+08 3.4147e+05 v TotEner 84791 6.295e+05 3.4164e+05 2.4857e+05 v temperature 53.523 533.94 397.78 337.23 v Density 0.38184 5.4621 0.94874 1.0901 v TurbVisc 8.7575e-19 0.064089 0.010077 0.028655 v CourantNb 1.3104e-05 44.106 0.39684 0.0076075 v FourierNb 4.5256e-05 202.15 1.82 0.090727 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 53.688 533.94 402.16 421.78 v Boundary Density 0.38196 5.4499 0.99696 0.90015 v Yplus 0 47.877 2.4593 0.96557 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8342e-05 44.694 0.48707 0.010638 INSTANT 0.159285525E-01 TIME STEP NUMBER 30234 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.682569098E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560750421E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123737648E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58438E+02 Friction velocity uk : 0.10335E+01 0.58438E+02 Dimensionless distance yplus : 0.20543E-01 0.47930E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14428E-01 0.12684E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60130E+03 2 0.23483E-06 0.85646E+02 0.22335E+03 c Velocity[X] 0.12851E+01 c Velocity[Y] 0.10878E+02 c Velocity[Z] 0.73483E+02 c Pressure 0.76200E-01 10 0.75037E-08 0.60901E+07 0.64957E+02 c k 0.24975E+04 2 0.25453E-06 0.27648E+06 0.26347E+04 c omega 0.81518E+09 1 0.51348E-08 0.45257E+12 0.49257E+02 c TotEner 0.24232E+06 1 0.11682E-05 0.90794E+07 0.32800E+02 c temperature 0.00000E+00 0 0.00000E+00 0.23594E+02 0.39180E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9456e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.28 229.28 0.0017855 0.0012266 v Velocity[Y] -0.12986 701.9 250.57 81.097 v Velocity[Z] -19.148 373.79 25.501 1.982 v ǁVelocityǁ 0.22937 701.9 260.51 83.836 v Pressure 48854 1.1024e+05 1.0344e+05 1.0416e+05 v k 1.1761e-08 43955 915.4 355.36 v omega 154.7 9.6786e+09 1.8461e+08 3.4147e+05 v TotEner 84669 6.295e+05 3.4164e+05 2.4857e+05 v temperature 53.357 533.94 397.78 337.23 v Density 0.38172 5.4746 0.94874 1.0901 v TurbVisc 8.7573e-19 0.064089 0.010077 0.028655 v CourantNb 1.3101e-05 44.114 0.39691 0.0076077 v FourierNb 4.5259e-05 202.11 1.8198 0.090728 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 53.523 533.94 402.15 421.78 v Boundary Density 0.38184 5.4621 0.99712 0.90019 v Yplus 0 47.93 2.4596 0.96573 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8338e-05 44.701 0.48714 0.010639 INSTANT 0.159288156E-01 TIME STEP NUMBER 30235 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.684222795E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560749060E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123702020E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58441E+02 Friction velocity uk : 0.10335E+01 0.58441E+02 Dimensionless distance yplus : 0.20543E-01 0.47984E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14428E-01 0.12687E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60130E+03 2 0.23475E-06 0.86777E+02 0.22482E+03 c Velocity[X] 0.12968E+01 c Velocity[Y] 0.10878E+02 c Velocity[Z] 0.74603E+02 c Pressure 0.76204E-01 10 0.69249E-08 0.61944E+07 0.65511E+02 c k 0.24981E+04 2 0.25725E-06 0.28165E+06 0.26588E+04 c omega 0.81518E+09 1 0.44214E-08 0.32174E+12 0.41532E+02 c TotEner 0.24232E+06 1 0.11706E-05 0.91944E+07 0.33007E+02 c temperature 0.00000E+00 0 0.00000E+00 0.23979E+02 0.39499E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9451e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.3 229.3 0.0017822 0.001229 v Velocity[Y] -0.12986 701.9 250.57 81.098 v Velocity[Z] -19.147 373.95 25.507 1.9822 v ǁVelocityǁ 0.22941 701.9 260.51 83.837 v Pressure 48837 1.1024e+05 1.0344e+05 1.0416e+05 v k 1.1761e-08 43982 915.47 355.36 v omega 154.7 9.6786e+09 1.8461e+08 3.4147e+05 v TotEner 84545 6.295e+05 3.4164e+05 2.4857e+05 v temperature 53.188 533.94 397.77 337.23 v Density 0.3816 5.4872 0.94873 1.0901 v TurbVisc 8.7571e-19 0.064088 0.010077 0.028655 v CourantNb 1.3099e-05 44.122 0.39697 0.0076078 v FourierNb 4.5263e-05 202.06 1.8196 0.090729 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 53.357 533.94 402.14 421.78 v Boundary Density 0.38172 5.4746 0.99727 0.90022 v Yplus 0 47.984 2.4598 0.96588 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8334e-05 44.708 0.48721 0.010639 INSTANT 0.159290786E-01 TIME STEP NUMBER 30236 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.685880986E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560747858E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123665393E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58445E+02 Friction velocity uk : 0.10335E+01 0.58445E+02 Dimensionless distance yplus : 0.20543E-01 0.48039E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14428E-01 0.12690E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60131E+03 2 0.23467E-06 0.87947E+02 0.22633E+03 c Velocity[X] 0.13091E+01 c Velocity[Y] 0.10892E+02 c Velocity[Z] 0.75746E+02 c Pressure 0.76208E-01 10 0.69540E-08 0.63014E+07 0.66075E+02 c k 0.24988E+04 2 0.26006E-06 0.28703E+06 0.26836E+04 c omega 0.81518E+09 1 0.43652E-08 0.31370E+12 0.41009E+02 c TotEner 0.24232E+06 1 0.11731E-05 0.93164E+07 0.33225E+02 c temperature 0.00000E+00 0 0.00000E+00 0.24376E+02 0.39824E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9447e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.33 229.33 0.0017789 0.0012315 v Velocity[Y] -0.12986 701.9 250.57 81.099 v Velocity[Z] -19.147 374.12 25.513 1.9825 v ǁVelocityǁ 0.22945 701.9 260.51 83.838 v Pressure 48821 1.1024e+05 1.0344e+05 1.0416e+05 v k 1.176e-08 44009 915.55 355.36 v omega 154.71 9.6786e+09 1.8461e+08 3.4147e+05 v TotEner 84420 6.295e+05 3.4164e+05 2.4857e+05 v temperature 53.018 533.94 397.77 337.23 v Density 0.38148 5.5 0.94873 1.0901 v TurbVisc 8.7569e-19 0.064088 0.010077 0.028655 v CourantNb 1.3096e-05 44.13 0.39704 0.007608 v FourierNb 4.5266e-05 202.02 1.8194 0.09073 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 53.188 533.94 402.13 421.78 v Boundary Density 0.3816 5.4872 0.99743 0.90025 v Yplus 0 48.039 2.46 0.96604 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8331e-05 44.714 0.48728 0.010639 INSTANT 0.159293417E-01 TIME STEP NUMBER 30237 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.687542345E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560746821E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123627748E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58449E+02 Friction velocity uk : 0.10335E+01 0.58449E+02 Dimensionless distance yplus : 0.20543E-01 0.48094E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14428E-01 0.12692E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60131E+03 2 0.23460E-06 0.89160E+02 0.22788E+03 c Velocity[X] 0.13220E+01 c Velocity[Y] 0.10925E+02 c Velocity[Z] 0.76913E+02 c Pressure 0.76212E-01 8 0.99875E-08 0.64113E+07 0.66648E+02 c k 0.24994E+04 2 0.26295E-06 0.29259E+06 0.27090E+04 c omega 0.81518E+09 1 0.46355E-08 0.43294E+12 0.48177E+02 c TotEner 0.24232E+06 1 0.11758E-05 0.94467E+07 0.33456E+02 c temperature 0.00000E+00 0 0.00000E+00 0.24783E+02 0.40156E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9442e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.36 229.36 0.0017755 0.0012339 v Velocity[Y] -0.12985 701.9 250.57 81.1 v Velocity[Z] -19.147 374.28 25.519 1.9827 v ǁVelocityǁ 0.22949 701.9 260.52 83.839 v Pressure 48804 1.1024e+05 1.0344e+05 1.0416e+05 v k 1.176e-08 44036 915.63 355.36 v omega 154.71 9.6786e+09 1.8461e+08 3.4147e+05 v TotEner 84294 6.295e+05 3.4164e+05 2.4857e+05 v temperature 52.846 533.94 397.77 337.23 v Density 0.38136 5.5131 0.94873 1.0901 v TurbVisc 8.7566e-19 0.064088 0.010077 0.028655 v CourantNb 1.3093e-05 44.139 0.39711 0.0076081 v FourierNb 4.5269e-05 201.97 1.8192 0.090731 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 53.018 533.94 402.12 421.77 v Boundary Density 0.38148 5.5 0.99759 0.90029 v Yplus 0 48.094 2.4603 0.9662 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8327e-05 44.721 0.48735 0.010639 INSTANT 0.159296047E-01 TIME STEP NUMBER 30238 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.689205539E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560745953E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123589062E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58452E+02 Friction velocity uk : 0.10335E+01 0.58452E+02 Dimensionless distance yplus : 0.20543E-01 0.48150E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14428E-01 0.12695E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60131E+03 2 0.23452E-06 0.90397E+02 0.22945E+03 c Velocity[X] 0.13355E+01 c Velocity[Y] 0.10957E+02 c Velocity[Z] 0.78104E+02 c Pressure 0.76216E-01 8 0.99641E-08 0.65241E+07 0.67232E+02 c k 0.25001E+04 2 0.26591E-06 0.29825E+06 0.27347E+04 c omega 0.81518E+09 1 0.44169E-08 0.46539E+12 0.49950E+02 c TotEner 0.24233E+06 1 0.11785E-05 0.95784E+07 0.33689E+02 c temperature 0.00000E+00 0 0.00000E+00 0.25200E+02 0.40492E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9438e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.38 229.38 0.0017721 0.0012363 v Velocity[Y] -0.12985 701.9 250.57 81.101 v Velocity[Z] -19.146 374.44 25.525 1.9829 v ǁVelocityǁ 0.22953 701.9 260.52 83.84 v Pressure 48787 1.1024e+05 1.0344e+05 1.0416e+05 v k 1.176e-08 44063 915.71 355.36 v omega 154.72 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 84166 6.295e+05 3.4164e+05 2.4857e+05 v temperature 52.672 533.94 397.77 337.23 v Density 0.38123 5.5263 0.94872 1.0901 v TurbVisc 8.7564e-19 0.064087 0.010077 0.028656 v CourantNb 1.309e-05 44.147 0.39718 0.0076083 v FourierNb 4.5273e-05 201.93 1.819 0.090732 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 52.846 533.94 402.11 421.77 v Boundary Density 0.38136 5.5131 0.99775 0.90032 v Yplus 0 48.15 2.4605 0.96637 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8323e-05 44.728 0.48742 0.010639 INSTANT 0.159298678E-01 TIME STEP NUMBER 30239 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.690869227E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560745254E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123549316E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58456E+02 Friction velocity uk : 0.10335E+01 0.58456E+02 Dimensionless distance yplus : 0.20543E-01 0.48207E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14428E-01 0.12698E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60131E+03 2 0.23444E-06 0.91580E+02 0.23095E+03 c Velocity[X] 0.13497E+01 c Velocity[Y] 0.10910E+02 c Velocity[Z] 0.79320E+02 c Pressure 0.76220E-01 10 0.71003E-08 0.66395E+07 0.67824E+02 c k 0.25008E+04 2 0.26891E-06 0.30385E+06 0.27597E+04 c omega 0.81518E+09 1 0.44198E-08 0.47510E+12 0.50469E+02 c TotEner 0.24233E+06 1 0.11811E-05 0.96912E+07 0.33887E+02 c temperature 0.00000E+00 0 0.00000E+00 0.25620E+02 0.40827E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9433e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.41 229.41 0.0017687 0.0012388 v Velocity[Y] -0.12985 701.9 250.57 81.102 v Velocity[Z] -19.146 374.61 25.531 1.9831 v ǁVelocityǁ 0.22957 701.9 260.53 83.841 v Pressure 48769 1.1024e+05 1.0344e+05 1.0416e+05 v k 1.1759e-08 44091 915.79 355.36 v omega 154.72 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 84037 6.295e+05 3.4164e+05 2.4857e+05 v temperature 52.497 533.94 397.76 337.23 v Density 0.38111 5.5396 0.94872 1.0901 v TurbVisc 8.7562e-19 0.064087 0.010078 0.028656 v CourantNb 1.3087e-05 44.155 0.39725 0.0076084 v FourierNb 4.5276e-05 201.88 1.8188 0.090733 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 52.672 533.94 402.09 421.77 v Boundary Density 0.38123 5.5263 0.99792 0.90035 v Yplus 0 48.207 2.4608 0.96653 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8319e-05 44.735 0.48749 0.01064 INSTANT 0.159301308E-01 TIME STEP NUMBER 30240 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.692532064E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560744720E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123508485E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58460E+02 Friction velocity uk : 0.10335E+01 0.58460E+02 Dimensionless distance yplus : 0.20543E-01 0.48264E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14428E-01 0.12701E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60132E+03 2 0.23437E-06 0.92816E+02 0.23250E+03 c Velocity[X] 0.13644E+01 c Velocity[Y] 0.10890E+02 c Velocity[Z] 0.80561E+02 c Pressure 0.76224E-01 10 0.69930E-08 0.67581E+07 0.68427E+02 c k 0.25015E+04 2 0.27201E-06 0.30963E+06 0.27853E+04 c omega 0.81518E+09 1 0.39619E-08 0.34751E+12 0.43163E+02 c TotEner 0.24233E+06 1 0.11839E-05 0.98174E+07 0.34107E+02 c temperature 0.00000E+00 0 0.00000E+00 0.26054E+02 0.41172E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9429e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.44 229.44 0.0017654 0.0012412 v Velocity[Y] -0.12985 701.9 250.57 81.103 v Velocity[Z] -19.145 374.77 25.537 1.9833 v ǁVelocityǁ 0.22961 701.9 260.53 83.842 v Pressure 48752 1.1024e+05 1.0343e+05 1.0416e+05 v k 1.1759e-08 44119 915.87 355.36 v omega 154.73 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 83907 6.295e+05 3.4164e+05 2.4857e+05 v temperature 52.32 533.94 397.76 337.23 v Density 0.38099 5.5532 0.94872 1.0901 v TurbVisc 8.756e-19 0.064086 0.010078 0.028656 v CourantNb 1.3084e-05 44.163 0.39732 0.0076085 v FourierNb 4.5279e-05 201.84 1.8186 0.090734 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 52.497 533.94 402.08 421.77 v Boundary Density 0.38111 5.5396 0.99808 0.90039 v Yplus 0 48.264 2.461 0.9667 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8315e-05 44.742 0.48756 0.01064 INSTANT 0.159303939E-01 TIME STEP NUMBER 30241 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.694192700E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560744345E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123466546E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58464E+02 Friction velocity uk : 0.10335E+01 0.58464E+02 Dimensionless distance yplus : 0.20543E-01 0.48323E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14428E-01 0.12704E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60132E+03 2 0.23429E-06 0.94091E+02 0.23409E+03 c Velocity[X] 0.13799E+01 c Velocity[Y] 0.10881E+02 c Velocity[Z] 0.81829E+02 c Pressure 0.76229E-01 10 0.74796E-08 0.68797E+07 0.69040E+02 c k 0.25022E+04 2 0.27520E-06 0.31562E+06 0.28117E+04 c omega 0.81518E+09 1 0.38642E-08 0.31905E+12 0.41357E+02 c TotEner 0.24233E+06 1 0.11869E-05 0.99488E+07 0.34334E+02 c temperature 0.00000E+00 0 0.00000E+00 0.26498E+02 0.41522E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9424e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.46 229.46 0.0017621 0.0012436 v Velocity[Y] -0.12985 701.9 250.58 81.104 v Velocity[Z] -19.145 374.94 25.543 1.9835 v ǁVelocityǁ 0.22965 701.9 260.54 83.843 v Pressure 48735 1.1024e+05 1.0343e+05 1.0416e+05 v k 1.1759e-08 44147 915.95 355.36 v omega 154.73 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 83775 6.295e+05 3.4164e+05 2.4857e+05 v temperature 52.14 533.94 397.76 337.23 v Density 0.38086 5.567 0.94871 1.0901 v TurbVisc 8.7558e-19 0.064086 0.010078 0.028656 v CourantNb 1.3081e-05 44.172 0.39739 0.0076087 v FourierNb 4.5283e-05 201.79 1.8184 0.090735 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 52.32 533.94 402.07 421.77 v Boundary Density 0.38099 5.5532 0.99825 0.90042 v Yplus 0 48.323 2.4613 0.96686 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8311e-05 44.749 0.48763 0.01064 INSTANT 0.159306570E-01 TIME STEP NUMBER 30242 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.695849780E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560744117E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123423475E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58467E+02 Friction velocity uk : 0.10335E+01 0.58467E+02 Dimensionless distance yplus : 0.20542E-01 0.48382E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14428E-01 0.12707E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60132E+03 2 0.23422E-06 0.95394E+02 0.23570E+03 c Velocity[X] 0.13961E+01 c Velocity[Y] 0.10873E+02 c Velocity[Z] 0.83125E+02 c Pressure 0.76233E-01 10 0.71676E-08 0.70049E+07 0.69665E+02 c k 0.25029E+04 2 0.27847E-06 0.32178E+06 0.28385E+04 c omega 0.81519E+09 1 0.37564E-08 0.27907E+12 0.38679E+02 c TotEner 0.24233E+06 1 0.11899E-05 0.10084E+08 0.34567E+02 c temperature 0.00000E+00 0 0.00000E+00 0.26954E+02 0.41877E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9419e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.49 229.49 0.0017586 0.001246 v Velocity[Y] -0.12985 701.9 250.58 81.105 v Velocity[Z] -19.144 375.1 25.55 1.9838 v ǁVelocityǁ 0.22969 701.9 260.54 83.844 v Pressure 48718 1.1024e+05 1.0343e+05 1.0416e+05 v k 1.1759e-08 44175 916.04 355.36 v omega 154.74 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 83642 6.295e+05 3.4164e+05 2.4857e+05 v temperature 51.959 533.94 397.76 337.23 v Density 0.38074 5.5811 0.94871 1.0901 v TurbVisc 8.7556e-19 0.064086 0.010078 0.028656 v CourantNb 1.3078e-05 44.18 0.39746 0.0076088 v FourierNb 4.5286e-05 201.75 1.8182 0.090736 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 52.14 533.94 402.06 421.76 v Boundary Density 0.38086 5.567 0.99842 0.90046 v Yplus 0 48.382 2.4615 0.96703 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8307e-05 44.756 0.4877 0.01064 INSTANT 0.159309200E-01 TIME STEP NUMBER 30243 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.697501949E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560744037E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123379246E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58471E+02 Friction velocity uk : 0.10335E+01 0.58471E+02 Dimensionless distance yplus : 0.20542E-01 0.48442E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14428E-01 0.12710E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60132E+03 2 0.23415E-06 0.96736E+02 0.23735E+03 c Velocity[X] 0.14130E+01 c Velocity[Y] 0.10876E+02 c Velocity[Z] 0.84448E+02 c Pressure 0.76237E-01 10 0.71807E-08 0.71335E+07 0.70302E+02 c k 0.25036E+04 2 0.28185E-06 0.32815E+06 0.28659E+04 c omega 0.81519E+09 1 0.36325E-08 0.29433E+12 0.39723E+02 c TotEner 0.24233E+06 1 0.11930E-05 0.10226E+08 0.34809E+02 c temperature 0.00000E+00 0 0.00000E+00 0.27423E+02 0.42240E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9415e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.52 229.52 0.001755 0.0012484 v Velocity[Y] -0.12984 701.9 250.58 81.106 v Velocity[Z] -19.144 375.27 25.556 1.984 v ǁVelocityǁ 0.22972 701.9 260.55 83.845 v Pressure 48701 1.1024e+05 1.0343e+05 1.0416e+05 v k 1.1758e-08 44203 916.12 355.36 v omega 154.74 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 83507 6.295e+05 3.4164e+05 2.4857e+05 v temperature 51.776 533.94 397.76 337.23 v Density 0.38062 5.5953 0.9487 1.0901 v TurbVisc 8.7554e-19 0.064085 0.010078 0.028656 v CourantNb 1.3075e-05 44.188 0.39753 0.007609 v FourierNb 4.529e-05 201.7 1.818 0.090738 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 51.959 533.94 402.05 421.76 v Boundary Density 0.38074 5.5811 0.99859 0.9005 v Yplus 0 48.442 2.4618 0.96721 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8302e-05 44.763 0.48777 0.01064 INSTANT 0.159311831E-01 TIME STEP NUMBER 30244 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.699147851E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560744094E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123333833E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58475E+02 Friction velocity uk : 0.10335E+01 0.58475E+02 Dimensionless distance yplus : 0.20542E-01 0.48503E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14428E-01 0.12713E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60133E+03 2 0.23407E-06 0.98104E+02 0.23902E+03 c Velocity[X] 0.14308E+01 c Velocity[Y] 0.10875E+02 c Velocity[Z] 0.85799E+02 c Pressure 0.76241E-01 10 0.69383E-08 0.72656E+07 0.70950E+02 c k 0.25043E+04 2 0.28531E-06 0.33470E+06 0.28939E+04 c omega 0.81519E+09 1 0.40198E-08 0.33154E+12 0.42159E+02 c TotEner 0.24233E+06 1 0.11963E-05 0.10370E+08 0.35054E+02 c temperature 0.00000E+00 0 0.00000E+00 0.27903E+02 0.42607E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.941e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.54 229.54 0.0017513 0.0012508 v Velocity[Y] -0.12984 701.9 250.58 81.107 v Velocity[Z] -19.143 375.44 25.562 1.9842 v ǁVelocityǁ 0.22976 701.9 260.55 83.846 v Pressure 48683 1.1024e+05 1.0343e+05 1.0416e+05 v k 1.1758e-08 44232 916.21 355.36 v omega 154.75 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 83371 6.295e+05 3.4164e+05 2.4857e+05 v temperature 51.591 533.94 397.75 337.23 v Density 0.38049 5.6097 0.9487 1.0901 v TurbVisc 8.7552e-19 0.064085 0.010078 0.028657 v CourantNb 1.3072e-05 44.197 0.3976 0.0076091 v FourierNb 4.5294e-05 201.66 1.8178 0.090739 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 51.776 533.94 402.04 421.76 v Boundary Density 0.38062 5.5953 0.99877 0.90053 v Yplus 0 48.503 2.462 0.96738 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8298e-05 44.77 0.48784 0.010641 INSTANT 0.159314461E-01 TIME STEP NUMBER 30245 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.700786130E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560744265E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123287208E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58479E+02 Friction velocity uk : 0.10335E+01 0.58479E+02 Dimensionless distance yplus : 0.20542E-01 0.48565E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14428E-01 0.12716E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60133E+03 2 0.23400E-06 0.99494E+02 0.24071E+03 c Velocity[X] 0.14493E+01 c Velocity[Y] 0.10866E+02 c Velocity[Z] 0.87179E+02 c Pressure 0.76245E-01 10 0.71196E-08 0.74016E+07 0.71611E+02 c k 0.25050E+04 2 0.28887E-06 0.34137E+06 0.29220E+04 c omega 0.81519E+09 1 0.38290E-08 0.27538E+12 0.38423E+02 c TotEner 0.24234E+06 1 0.11996E-05 0.10517E+08 0.35300E+02 c temperature 0.00000E+00 0 0.00000E+00 0.28394E+02 0.42981E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9405e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.57 229.57 0.0017476 0.0012531 v Velocity[Y] -0.12984 701.9 250.58 81.108 v Velocity[Z] -19.143 375.61 25.568 1.9844 v ǁVelocityǁ 0.2298 701.9 260.56 83.847 v Pressure 48666 1.1024e+05 1.0343e+05 1.0416e+05 v k 1.1758e-08 44261 916.29 355.36 v omega 154.75 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 83234 6.295e+05 3.4164e+05 2.4857e+05 v temperature 51.404 533.94 397.75 337.23 v Density 0.38037 5.6244 0.9487 1.0901 v TurbVisc 8.7549e-19 0.064084 0.010078 0.028657 v CourantNb 1.3069e-05 44.205 0.39767 0.0076093 v FourierNb 4.5297e-05 201.62 1.8176 0.09074 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 51.591 533.94 402.02 421.76 v Boundary Density 0.38049 5.6097 0.99895 0.90057 v Yplus 0 48.565 2.4623 0.96756 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8294e-05 44.777 0.48791 0.010641 INSTANT 0.159317092E-01 TIME STEP NUMBER 30246 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.702415433E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560744531E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123239342E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58483E+02 Friction velocity uk : 0.10335E+01 0.58483E+02 Dimensionless distance yplus : 0.20542E-01 0.48627E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14427E-01 0.12719E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60133E+03 2 0.23393E-06 0.10093E+03 0.24243E+03 c Velocity[X] 0.14688E+01 c Velocity[Y] 0.10871E+02 c Velocity[Z] 0.88589E+02 c Pressure 0.76249E-01 10 0.77038E-08 0.75409E+07 0.72282E+02 c k 0.25058E+04 2 0.29253E-06 0.34829E+06 0.29509E+04 c omega 0.81519E+09 1 0.39742E-08 0.27704E+12 0.38539E+02 c TotEner 0.24234E+06 1 0.12030E-05 0.10669E+08 0.35555E+02 c temperature 0.00000E+00 0 0.00000E+00 0.28898E+02 0.43361E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9401e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.6 229.6 0.0017439 0.0012555 v Velocity[Y] -0.12984 701.9 250.58 81.109 v Velocity[Z] -19.142 375.78 25.575 1.9846 v ǁVelocityǁ 0.22983 701.9 260.56 83.847 v Pressure 48649 1.1024e+05 1.0342e+05 1.0416e+05 v k 1.1757e-08 44290 916.38 355.36 v omega 154.76 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 83095 6.295e+05 3.4164e+05 2.4857e+05 v temperature 51.215 533.94 397.75 337.23 v Density 0.38024 5.6393 0.94869 1.0901 v TurbVisc 8.7547e-19 0.064084 0.010078 0.028657 v CourantNb 1.3066e-05 44.214 0.39774 0.0076094 v FourierNb 4.5301e-05 201.57 1.8174 0.090741 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 51.404 533.94 402.01 421.75 v Boundary Density 0.38037 5.6244 0.99913 0.90061 v Yplus 0 48.627 2.4626 0.96773 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8289e-05 44.784 0.48798 0.010641 INSTANT 0.159319722E-01 TIME STEP NUMBER 30247 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.704034408E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560744870E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123190205E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58486E+02 Friction velocity uk : 0.10335E+01 0.58486E+02 Dimensionless distance yplus : 0.20542E-01 0.48691E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14427E-01 0.12722E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60133E+03 2 0.23386E-06 0.10239E+03 0.24418E+03 c Velocity[X] 0.14891E+01 c Velocity[Y] 0.10869E+02 c Velocity[Z] 0.90029E+02 c Pressure 0.76253E-01 10 0.73243E-08 0.76846E+07 0.72967E+02 c k 0.25065E+04 2 0.29629E-06 0.35538E+06 0.29803E+04 c omega 0.81519E+09 1 0.37398E-08 0.26912E+12 0.37984E+02 c TotEner 0.24234E+06 1 0.12066E-05 0.10825E+08 0.35814E+02 c temperature 0.00000E+00 0 0.00000E+00 0.29415E+02 0.43747E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9396e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.63 229.63 0.0017401 0.0012578 v Velocity[Y] -0.12984 701.9 250.58 81.11 v Velocity[Z] -19.142 375.95 25.581 1.9849 v ǁVelocityǁ 0.22987 701.9 260.56 83.848 v Pressure 48631 1.1024e+05 1.0342e+05 1.0416e+05 v k 1.1757e-08 44319 916.47 355.36 v omega 154.76 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 82954 6.295e+05 3.4164e+05 2.4857e+05 v temperature 51.024 533.94 397.75 337.23 v Density 0.38012 5.6545 0.94869 1.0901 v TurbVisc 8.7545e-19 0.064084 0.010078 0.028657 v CourantNb 1.3062e-05 44.222 0.39781 0.0076096 v FourierNb 4.5304e-05 201.53 1.8172 0.090742 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 51.215 533.94 402 421.75 v Boundary Density 0.38024 5.6393 0.99931 0.90065 v Yplus 0 48.691 2.4629 0.96792 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8285e-05 44.791 0.48805 0.010641 INSTANT 0.159322353E-01 TIME STEP NUMBER 30248 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.705641711E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560745268E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123139766E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10335E+01 0.58490E+02 Friction velocity uk : 0.10335E+01 0.58490E+02 Dimensionless distance yplus : 0.20542E-01 0.48755E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14427E-01 0.12725E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60134E+03 2 0.23379E-06 0.10388E+03 0.24594E+03 c Velocity[X] 0.15105E+01 c Velocity[Y] 0.10866E+02 c Velocity[Z] 0.91500E+02 c Pressure 0.76257E-01 10 0.75949E-08 0.78323E+07 0.73665E+02 c k 0.25073E+04 2 0.30016E-06 0.36267E+06 0.30101E+04 c omega 0.81519E+09 1 0.38723E-08 0.29893E+12 0.40033E+02 c TotEner 0.24234E+06 1 0.12103E-05 0.10984E+08 0.36076E+02 c temperature 0.00000E+00 0 0.00000E+00 0.29945E+02 0.44139E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9392e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.65 229.65 0.0017363 0.0012601 v Velocity[Y] -0.12984 701.9 250.58 81.11 v Velocity[Z] -19.141 376.12 25.587 1.9851 v ǁVelocityǁ 0.22991 701.9 260.57 83.849 v Pressure 48614 1.1024e+05 1.0342e+05 1.0416e+05 v k 1.1757e-08 44349 916.57 355.36 v omega 154.77 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 82812 6.295e+05 3.4164e+05 2.4857e+05 v temperature 50.831 533.94 397.74 337.23 v Density 0.37999 5.6699 0.94869 1.0901 v TurbVisc 8.7543e-19 0.064083 0.010079 0.028657 v CourantNb 1.3059e-05 44.23 0.39788 0.0076097 v FourierNb 4.5308e-05 201.48 1.8171 0.090743 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 51.024 533.94 401.99 421.75 v Boundary Density 0.38012 5.6545 0.9995 0.90069 v Yplus 0 48.755 2.4631 0.9681 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8281e-05 44.799 0.48812 0.010641 INSTANT 0.159324984E-01 TIME STEP NUMBER 30249 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.707236001E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560745709E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123087993E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58494E+02 Friction velocity uk : 0.10334E+01 0.58494E+02 Dimensionless distance yplus : 0.20542E-01 0.48821E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14427E-01 0.12728E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60134E+03 2 0.23372E-06 0.10540E+03 0.24774E+03 c Velocity[X] 0.15328E+01 c Velocity[Y] 0.10863E+02 c Velocity[Z] 0.93004E+02 c Pressure 0.76261E-01 10 0.81194E-08 0.79842E+07 0.74376E+02 c k 0.25080E+04 2 0.30413E-06 0.37015E+06 0.30404E+04 c omega 0.81519E+09 1 0.33522E-08 0.21704E+12 0.34111E+02 c TotEner 0.24234E+06 1 0.12141E-05 0.11147E+08 0.36343E+02 c temperature 0.00000E+00 0 0.00000E+00 0.30489E+02 0.44538E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9387e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.68 229.68 0.0017325 0.0012625 v Velocity[Y] -0.12983 701.9 250.58 81.111 v Velocity[Z] -19.141 376.29 25.594 1.9853 v ǁVelocityǁ 0.22994 701.9 260.57 83.85 v Pressure 48596 1.1024e+05 1.0342e+05 1.0416e+05 v k 1.1757e-08 44378 916.66 355.36 v omega 154.77 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 82668 6.295e+05 3.4164e+05 2.4858e+05 v temperature 50.636 533.94 397.74 337.23 v Density 0.37987 5.6855 0.94868 1.0901 v TurbVisc 8.7541e-19 0.064083 0.010079 0.028657 v CourantNb 1.3056e-05 44.239 0.39795 0.0076099 v FourierNb 4.5312e-05 201.44 1.8169 0.090744 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 50.831 533.94 401.97 421.75 v Boundary Density 0.37999 5.6699 0.99968 0.90073 v Yplus 0 48.821 2.4634 0.96828 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8276e-05 44.806 0.48819 0.010642 INSTANT 0.159327614E-01 TIME STEP NUMBER 30250 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.708815945E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560746193E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.123034853E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58498E+02 Friction velocity uk : 0.10334E+01 0.58498E+02 Dimensionless distance yplus : 0.20542E-01 0.48887E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14427E-01 0.12731E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60134E+03 2 0.23365E-06 0.10696E+03 0.24956E+03 c Velocity[X] 0.15563E+01 c Velocity[Y] 0.10866E+02 c Velocity[Z] 0.94540E+02 c Pressure 0.76265E-01 10 0.83086E-08 0.81405E+07 0.75101E+02 c k 0.25088E+04 2 0.30823E-06 0.37787E+06 0.30713E+04 c omega 0.81519E+09 1 0.39628E-08 0.32101E+12 0.41484E+02 c TotEner 0.24234E+06 1 0.12180E-05 0.11316E+08 0.36617E+02 c temperature 0.00000E+00 0 0.00000E+00 0.31046E+02 0.44943E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9382e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.71 229.71 0.0017287 0.0012648 v Velocity[Y] -0.12983 701.9 250.58 81.112 v Velocity[Z] -19.14 376.46 25.6 1.9855 v ǁVelocityǁ 0.22998 701.9 260.58 83.851 v Pressure 48579 1.1024e+05 1.0342e+05 1.0416e+05 v k 1.1756e-08 44409 916.75 355.36 v omega 154.78 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 82523 6.295e+05 3.4164e+05 2.4858e+05 v temperature 50.438 533.94 397.74 337.23 v Density 0.37974 5.7014 0.94868 1.0901 v TurbVisc 8.7539e-19 0.064082 0.010079 0.028658 v CourantNb 1.3052e-05 44.247 0.39803 0.00761 v FourierNb 4.5316e-05 201.39 1.8167 0.090745 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 50.636 533.94 401.96 421.74 v Boundary Density 0.37987 5.6855 0.99987 0.90077 v Yplus 0 48.887 2.4637 0.96847 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8272e-05 44.813 0.48827 0.010642 INSTANT 0.159330245E-01 TIME STEP NUMBER 30251 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.710380221E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560746714E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122980311E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58502E+02 Friction velocity uk : 0.10334E+01 0.58502E+02 Dimensionless distance yplus : 0.20542E-01 0.48954E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14427E-01 0.12735E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60134E+03 2 0.23359E-06 0.10854E+03 0.25140E+03 c Velocity[X] 0.15808E+01 c Velocity[Y] 0.10853E+02 c Velocity[Z] 0.96110E+02 c Pressure 0.76270E-01 10 0.78446E-08 0.83017E+07 0.75841E+02 c k 0.25096E+04 2 0.31243E-06 0.38577E+06 0.31027E+04 c omega 0.81519E+09 1 0.35397E-08 0.25874E+12 0.37244E+02 c TotEner 0.24234E+06 1 0.12220E-05 0.11486E+08 0.36891E+02 c temperature 0.00000E+00 0 0.00000E+00 0.31618E+02 0.45355E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9378e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.73 229.73 0.0017248 0.0012671 v Velocity[Y] -0.12983 701.9 250.58 81.113 v Velocity[Z] -19.14 376.64 25.606 1.9857 v ǁVelocityǁ 0.23001 701.9 260.58 83.852 v Pressure 48561 1.1024e+05 1.0342e+05 1.0415e+05 v k 1.1756e-08 44439 916.85 355.36 v omega 154.78 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 82376 6.295e+05 3.4164e+05 2.4858e+05 v temperature 50.238 533.94 397.74 337.23 v Density 0.37961 5.7175 0.94868 1.0901 v TurbVisc 8.7537e-19 0.064082 0.010079 0.028658 v CourantNb 1.3049e-05 44.256 0.3981 0.0076102 v FourierNb 4.5319e-05 201.35 1.8165 0.090746 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 50.438 533.94 401.95 421.74 v Boundary Density 0.37974 5.7014 1.0001 0.90081 v Yplus 0 48.954 2.464 0.96866 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8267e-05 44.82 0.48834 0.010642 INSTANT 0.159332876E-01 TIME STEP NUMBER 30252 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.711927512E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560747272E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122924330E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58505E+02 Friction velocity uk : 0.10334E+01 0.58505E+02 Dimensionless distance yplus : 0.20541E-01 0.49023E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14427E-01 0.12738E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60135E+03 2 0.23352E-06 0.11018E+03 0.25328E+03 c Velocity[X] 0.16066E+01 c Velocity[Y] 0.10856E+02 c Velocity[Z] 0.97715E+02 c Pressure 0.76274E-01 10 0.91229E-08 0.84673E+07 0.76594E+02 c k 0.25104E+04 2 0.31675E-06 0.39393E+06 0.31347E+04 c omega 0.81519E+09 1 0.42551E-08 0.31469E+12 0.41074E+02 c TotEner 0.24235E+06 1 0.12262E-05 0.11664E+08 0.37176E+02 c temperature 0.00000E+00 0 0.00000E+00 0.32204E+02 0.45774E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9373e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.76 229.76 0.0017209 0.0012695 v Velocity[Y] -0.12983 701.9 250.58 81.114 v Velocity[Z] -19.14 376.81 25.613 1.986 v ǁVelocityǁ 0.23004 701.9 260.59 83.853 v Pressure 48543 1.1024e+05 1.0341e+05 1.0415e+05 v k 1.1756e-08 44469 916.94 355.36 v omega 154.79 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 82227 6.295e+05 3.4164e+05 2.4858e+05 v temperature 50.036 533.94 397.73 337.23 v Density 0.37949 5.734 0.94867 1.0901 v TurbVisc 8.7535e-19 0.064082 0.010079 0.028658 v CourantNb 1.3046e-05 44.265 0.39817 0.0076103 v FourierNb 4.5323e-05 201.31 1.8163 0.090747 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 50.238 533.94 401.93 421.74 v Boundary Density 0.37961 5.7175 1.0003 0.90085 v Yplus 0 49.023 2.4643 0.96886 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8262e-05 44.827 0.48841 0.010642 INSTANT 0.159335506E-01 TIME STEP NUMBER 30253 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.713456515E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560747870E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122866873E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58509E+02 Friction velocity uk : 0.10334E+01 0.58509E+02 Dimensionless distance yplus : 0.20541E-01 0.49092E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14427E-01 0.12741E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60135E+03 2 0.23345E-06 0.11185E+03 0.25520E+03 c Velocity[X] 0.16337E+01 c Velocity[Y] 0.10863E+02 c Velocity[Z] 0.99356E+02 c Pressure 0.76278E-01 10 0.85565E-08 0.86382E+07 0.77363E+02 c k 0.25112E+04 2 0.32120E-06 0.40233E+06 0.31673E+04 c omega 0.81519E+09 1 0.44793E-08 0.33393E+12 0.42311E+02 c TotEner 0.24235E+06 1 0.12306E-05 0.11848E+08 0.37468E+02 c temperature 0.00000E+00 0 0.00000E+00 0.32807E+02 0.46200E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9368e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.79 229.79 0.0017169 0.0012718 v Velocity[Y] -0.12983 701.9 250.58 81.115 v Velocity[Z] -19.139 376.99 25.619 1.9862 v ǁVelocityǁ 0.23008 701.9 260.59 83.854 v Pressure 48525 1.1024e+05 1.0341e+05 1.0415e+05 v k 1.1756e-08 44500 917.04 355.36 v omega 154.79 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 82077 6.295e+05 3.4164e+05 2.4858e+05 v temperature 49.832 533.94 397.73 337.23 v Density 0.37936 5.7506 0.94867 1.0901 v TurbVisc 8.7533e-19 0.064081 0.010079 0.028658 v CourantNb 1.3042e-05 44.273 0.39824 0.0076105 v FourierNb 4.5327e-05 201.26 1.8161 0.090748 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 50.036 533.94 401.92 421.74 v Boundary Density 0.37949 5.734 1.0005 0.90089 v Yplus 0 49.092 2.4646 0.96905 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8258e-05 44.834 0.48848 0.010642 INSTANT 0.159338137E-01 TIME STEP NUMBER 30254 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.714965939E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560748518E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122807900E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58513E+02 Friction velocity uk : 0.10334E+01 0.58513E+02 Dimensionless distance yplus : 0.20541E-01 0.49162E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14427E-01 0.12745E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60135E+03 2 0.23339E-06 0.11355E+03 0.25713E+03 c Velocity[X] 0.16621E+01 c Velocity[Y] 0.10856E+02 c Velocity[Z] 0.10103E+03 c Pressure 0.76282E-01 10 0.77305E-08 0.88143E+07 0.78147E+02 c k 0.25120E+04 2 0.32577E-06 0.41093E+06 0.32003E+04 c omega 0.81519E+09 1 0.42453E-08 0.30548E+12 0.40469E+02 c TotEner 0.24235E+06 1 0.12350E-05 0.12034E+08 0.37760E+02 c temperature 0.00000E+00 0 0.00000E+00 0.33424E+02 0.46633E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9364e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.82 229.82 0.0017128 0.0012741 v Velocity[Y] -0.12983 701.9 250.58 81.116 v Velocity[Z] -19.139 377.17 25.626 1.9864 v ǁVelocityǁ 0.23011 701.9 260.6 83.855 v Pressure 48508 1.1024e+05 1.0341e+05 1.0415e+05 v k 1.1755e-08 44531 917.14 355.36 v omega 154.8 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 81924 6.295e+05 3.4164e+05 2.4858e+05 v temperature 49.625 533.94 397.73 337.23 v Density 0.37923 5.7676 0.94867 1.0901 v TurbVisc 8.7531e-19 0.064081 0.010079 0.028658 v CourantNb 1.3039e-05 44.282 0.39831 0.0076106 v FourierNb 4.5331e-05 201.22 1.8159 0.09075 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 49.832 533.94 401.91 421.73 v Boundary Density 0.37936 5.7506 1.0007 0.90094 v Yplus 0 49.162 2.465 0.96925 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8253e-05 44.841 0.48855 0.010643 INSTANT 0.159340767E-01 TIME STEP NUMBER 30255 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.716454506E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560749222E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122747373E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58517E+02 Friction velocity uk : 0.10334E+01 0.58517E+02 Dimensionless distance yplus : 0.20541E-01 0.49234E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14427E-01 0.12748E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60135E+03 2 0.23332E-06 0.11530E+03 0.25910E+03 c Velocity[X] 0.16918E+01 c Velocity[Y] 0.10862E+02 c Velocity[Z] 0.10275E+03 c Pressure 0.76286E-01 10 0.74482E-08 0.89957E+07 0.78947E+02 c k 0.25128E+04 2 0.33048E-06 0.41983E+06 0.32341E+04 c omega 0.81519E+09 1 0.45846E-08 0.38754E+12 0.45581E+02 c TotEner 0.24235E+06 1 0.12397E-05 0.12228E+08 0.38063E+02 c temperature 0.00000E+00 0 0.00000E+00 0.34059E+02 0.47073E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9359e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.84 229.85 0.0017085 0.0012763 v Velocity[Y] -0.12983 701.9 250.58 81.117 v Velocity[Z] -19.138 377.34 25.633 1.9866 v ǁVelocityǁ 0.23014 701.9 260.6 83.856 v Pressure 48490 1.1024e+05 1.0341e+05 1.0415e+05 v k 1.1755e-08 44563 917.24 355.36 v omega 154.8 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 81770 6.295e+05 3.4164e+05 2.4858e+05 v temperature 49.416 533.94 397.73 337.24 v Density 0.3791 5.7849 0.94866 1.0901 v TurbVisc 8.7529e-19 0.064081 0.010079 0.028658 v CourantNb 1.3035e-05 44.29 0.39839 0.0076108 v FourierNb 4.5335e-05 201.17 1.8157 0.090751 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 49.625 533.94 401.89 421.73 v Boundary Density 0.37923 5.7676 1.0009 0.90098 v Yplus 0 49.234 2.4653 0.96945 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8248e-05 44.849 0.48863 0.010643 INSTANT 0.159343398E-01 TIME STEP NUMBER 30256 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.717920953E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560749994E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122685247E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58521E+02 Friction velocity uk : 0.10334E+01 0.58521E+02 Dimensionless distance yplus : 0.20541E-01 0.49306E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14427E-01 0.12752E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60136E+03 2 0.23326E-06 0.11710E+03 0.26111E+03 c Velocity[X] 0.17231E+01 c Velocity[Y] 0.10877E+02 c Velocity[Z] 0.10450E+03 c Pressure 0.76290E-01 10 0.72595E-08 0.91829E+07 0.79765E+02 c k 0.25136E+04 2 0.33534E-06 0.42900E+06 0.32686E+04 c omega 0.81519E+09 1 0.40643E-08 0.29599E+12 0.39835E+02 c TotEner 0.24235E+06 1 0.12445E-05 0.12429E+08 0.38375E+02 c temperature 0.00000E+00 0 0.00000E+00 0.34711E+02 0.47522E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9354e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.87 229.87 0.0017042 0.0012786 v Velocity[Y] -0.12982 701.9 250.58 81.118 v Velocity[Z] -19.138 377.52 25.639 1.9869 v ǁVelocityǁ 0.23018 701.9 260.61 83.857 v Pressure 48472 1.1024e+05 1.0341e+05 1.0415e+05 v k 1.1755e-08 44594 917.34 355.36 v omega 154.81 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 81615 6.295e+05 3.4164e+05 2.4858e+05 v temperature 49.205 533.94 397.72 337.24 v Density 0.37897 5.8024 0.94866 1.0901 v TurbVisc 8.7527e-19 0.06408 0.01008 0.028658 v CourantNb 1.3032e-05 44.299 0.39846 0.0076109 v FourierNb 4.5339e-05 201.13 1.8155 0.090752 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 49.416 533.94 401.88 421.73 v Boundary Density 0.3791 5.7849 1.0011 0.90102 v Yplus 0 49.306 2.4656 0.96966 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8243e-05 44.856 0.4887 0.010643 INSTANT 0.159346029E-01 TIME STEP NUMBER 30257 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.719364033E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560750837E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122621480E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58525E+02 Friction velocity uk : 0.10334E+01 0.58525E+02 Dimensionless distance yplus : 0.20541E-01 0.49380E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14427E-01 0.12755E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60136E+03 2 0.23320E-06 0.11896E+03 0.26317E+03 c Velocity[X] 0.17559E+01 c Velocity[Y] 0.10902E+02 c Velocity[Z] 0.10630E+03 c Pressure 0.76294E-01 10 0.72349E-08 0.93758E+07 0.80598E+02 c k 0.25145E+04 2 0.34034E-06 0.43847E+06 0.33038E+04 c omega 0.81519E+09 1 0.48472E-08 0.45398E+12 0.49334E+02 c TotEner 0.24235E+06 1 0.12495E-05 0.12637E+08 0.38695E+02 c temperature 0.00000E+00 0 0.00000E+00 0.35381E+02 0.47978E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9349e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.9 229.9 0.0016997 0.0012808 v Velocity[Y] -0.12982 701.9 250.58 81.119 v Velocity[Z] -19.137 377.7 25.646 1.9871 v ǁVelocityǁ 0.23021 701.9 260.61 83.858 v Pressure 48454 1.1024e+05 1.0341e+05 1.0415e+05 v k 1.1755e-08 44626 917.44 355.36 v omega 154.81 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 81457 6.295e+05 3.4164e+05 2.4858e+05 v temperature 48.991 533.94 397.72 337.24 v Density 0.37884 5.8203 0.94866 1.0901 v TurbVisc 8.7525e-19 0.06408 0.01008 0.028659 v CourantNb 1.3028e-05 44.308 0.39853 0.0076111 v FourierNb 4.5342e-05 201.09 1.8153 0.090753 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 49.205 533.94 401.86 421.72 v Boundary Density 0.37897 5.8024 1.0013 0.90107 v Yplus 0 49.38 2.4659 0.96986 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8238e-05 44.863 0.48877 0.010643 INSTANT 0.159348659E-01 TIME STEP NUMBER 30258 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.720782514E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560751761E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122556025E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58529E+02 Friction velocity uk : 0.10334E+01 0.58529E+02 Dimensionless distance yplus : 0.20541E-01 0.49455E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14427E-01 0.12759E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60136E+03 2 0.23314E-06 0.12084E+03 0.26524E+03 c Velocity[X] 0.17904E+01 c Velocity[Y] 0.10912E+02 c Velocity[Z] 0.10813E+03 c Pressure 0.76299E-01 10 0.70973E-08 0.95754E+07 0.81452E+02 c k 0.25153E+04 2 0.34548E-06 0.44819E+06 0.33395E+04 c omega 0.81519E+09 1 0.49355E-08 0.44338E+12 0.48754E+02 c TotEner 0.24235E+06 1 0.12546E-05 0.12848E+08 0.39017E+02 c temperature 0.00000E+00 0 0.00000E+00 0.36069E+02 0.48442E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9345e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.93 229.93 0.001695 0.0012831 v Velocity[Y] -0.12982 701.9 250.58 81.12 v Velocity[Z] -19.137 377.88 25.653 1.9873 v ǁVelocityǁ 0.23024 701.9 260.62 83.859 v Pressure 48436 1.1024e+05 1.034e+05 1.0415e+05 v k 1.1754e-08 44658 917.54 355.37 v omega 154.82 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 81297 6.295e+05 3.4164e+05 2.4858e+05 v temperature 48.774 533.94 397.72 337.24 v Density 0.37871 5.8385 0.94865 1.0901 v TurbVisc 8.7523e-19 0.064079 0.01008 0.028659 v CourantNb 1.3024e-05 44.316 0.3986 0.0076112 v FourierNb 4.5346e-05 201.04 1.8151 0.090754 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 48.991 533.94 401.85 421.72 v Boundary Density 0.37884 5.8203 1.0015 0.90111 v Yplus 0 49.455 2.4663 0.97008 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8233e-05 44.87 0.48885 0.010643 INSTANT 0.159351290E-01 TIME STEP NUMBER 30259 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.722175187E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560752773E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122488836E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58533E+02 Friction velocity uk : 0.10334E+01 0.58533E+02 Dimensionless distance yplus : 0.20541E-01 0.49531E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14426E-01 0.12763E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60136E+03 2 0.23307E-06 0.12276E+03 0.26734E+03 c Velocity[X] 0.18267E+01 c Velocity[Y] 0.10920E+02 c Velocity[Z] 0.11001E+03 c Pressure 0.76303E-01 10 0.74850E-08 0.97807E+07 0.82320E+02 c k 0.25162E+04 2 0.35076E-06 0.45819E+06 0.33758E+04 c omega 0.81519E+09 1 0.44336E-08 0.38344E+12 0.45339E+02 c TotEner 0.24236E+06 1 0.12599E-05 0.13064E+08 0.39342E+02 c temperature 0.00000E+00 0 0.00000E+00 0.36774E+02 0.48913E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.934e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.96 229.96 0.0016902 0.0012853 v Velocity[Y] -0.12982 701.9 250.58 81.121 v Velocity[Z] -19.136 378.06 25.659 1.9875 v ǁVelocityǁ 0.23027 701.9 260.62 83.86 v Pressure 48418 1.1024e+05 1.034e+05 1.0415e+05 v k 1.1754e-08 44691 917.65 355.37 v omega 154.82 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 81136 6.295e+05 3.4164e+05 2.4858e+05 v temperature 48.555 533.94 397.72 337.24 v Density 0.37858 5.857 0.94865 1.0901 v TurbVisc 8.7521e-19 0.064079 0.01008 0.028659 v CourantNb 1.302e-05 44.325 0.39868 0.0076114 v FourierNb 4.535e-05 201 1.8149 0.090755 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 48.774 533.94 401.84 421.72 v Boundary Density 0.37871 5.8385 1.0017 0.90116 v Yplus 0 49.531 2.4666 0.97029 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8228e-05 44.877 0.48892 0.010644 INSTANT 0.159353921E-01 TIME STEP NUMBER 30260 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.723540858E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560753877E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122419864E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58536E+02 Friction velocity uk : 0.10334E+01 0.58536E+02 Dimensionless distance yplus : 0.20541E-01 0.49608E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14426E-01 0.12766E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60137E+03 2 0.23301E-06 0.12468E+03 0.26941E+03 c Velocity[X] 0.18647E+01 c Velocity[Y] 0.10878E+02 c Velocity[Z] 0.11193E+03 c Pressure 0.76307E-01 10 0.72549E-08 0.99928E+07 0.83208E+02 c k 0.25171E+04 2 0.35619E-06 0.46830E+06 0.34121E+04 c omega 0.81519E+09 1 0.54537E-08 0.46127E+12 0.49728E+02 c TotEner 0.24236E+06 1 0.12652E-05 0.13271E+08 0.39654E+02 c temperature 0.00000E+00 0 0.00000E+00 0.37494E+02 0.49389E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9335e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -229.98 229.98 0.0016853 0.0012875 v Velocity[Y] -0.12982 701.9 250.59 81.122 v Velocity[Z] -19.136 378.25 25.666 1.9878 v ǁVelocityǁ 0.2303 701.9 260.63 83.861 v Pressure 48400 1.1024e+05 1.034e+05 1.0415e+05 v k 1.1754e-08 44723 917.75 355.37 v omega 154.83 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 80972 6.295e+05 3.4164e+05 2.4858e+05 v temperature 48.334 533.94 397.71 337.24 v Density 0.37845 5.8758 0.94865 1.0901 v TurbVisc 8.7519e-19 0.064079 0.01008 0.028659 v CourantNb 1.3017e-05 44.334 0.39875 0.0076115 v FourierNb 4.5354e-05 200.95 1.8147 0.090756 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 48.555 533.94 401.82 421.72 v Boundary Density 0.37858 5.857 1.0019 0.90121 v Yplus 0 49.608 2.467 0.97051 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8223e-05 44.885 0.48899 0.010644 INSTANT 0.159356551E-01 TIME STEP NUMBER 30261 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.724878355E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560755072E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122349058E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58540E+02 Friction velocity uk : 0.10334E+01 0.58540E+02 Dimensionless distance yplus : 0.20541E-01 0.49687E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14426E-01 0.12770E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60137E+03 2 0.23296E-06 0.12667E+03 0.27155E+03 c Velocity[X] 0.19046E+01 c Velocity[Y] 0.10863E+02 c Velocity[Z] 0.11390E+03 c Pressure 0.76311E-01 10 0.78489E-08 0.10212E+08 0.84114E+02 c k 0.25180E+04 2 0.36181E-06 0.47885E+06 0.34496E+04 c omega 0.81519E+09 1 0.49661E-08 0.41737E+12 0.47302E+02 c TotEner 0.24236E+06 1 0.12708E-05 0.13493E+08 0.39984E+02 c temperature 0.00000E+00 0 0.00000E+00 0.38235E+02 0.49875E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.933e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.01 230.01 0.0016805 0.0012897 v Velocity[Y] -0.12982 701.9 250.59 81.123 v Velocity[Z] -19.135 378.43 25.673 1.988 v ǁVelocityǁ 0.23033 701.9 260.63 83.862 v Pressure 48381 1.1024e+05 1.034e+05 1.0415e+05 v k 1.1753e-08 44756 917.86 355.37 v omega 154.83 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 80807 6.295e+05 3.4164e+05 2.4858e+05 v temperature 48.109 533.94 397.71 337.24 v Density 0.37832 5.8949 0.94864 1.0901 v TurbVisc 8.7517e-19 0.064078 0.01008 0.028659 v CourantNb 1.3013e-05 44.343 0.39883 0.0076117 v FourierNb 4.5358e-05 200.91 1.8145 0.090757 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 48.334 533.94 401.81 421.71 v Boundary Density 0.37845 5.8758 1.0022 0.90126 v Yplus 0 49.687 2.4673 0.97073 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8217e-05 44.892 0.48907 0.010644 INSTANT 0.159359182E-01 TIME STEP NUMBER 30262 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.726186530E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560756358E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122276363E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58544E+02 Friction velocity uk : 0.10334E+01 0.58544E+02 Dimensionless distance yplus : 0.20540E-01 0.49767E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14426E-01 0.12774E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60137E+03 2 0.23290E-06 0.12872E+03 0.27374E+03 c Velocity[X] 0.19466E+01 c Velocity[Y] 0.10859E+02 c Velocity[Z] 0.11591E+03 c Pressure 0.76315E-01 10 0.80471E-08 0.10438E+08 0.85043E+02 c k 0.25189E+04 2 0.36760E-06 0.48979E+06 0.34880E+04 c omega 0.81519E+09 1 0.48090E-08 0.42576E+12 0.47776E+02 c TotEner 0.24236E+06 1 0.12766E-05 0.13725E+08 0.40325E+02 c temperature 0.00000E+00 0 0.00000E+00 0.38999E+02 0.50371E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9326e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.04 230.04 0.0016756 0.0012919 v Velocity[Y] -0.12982 701.9 250.59 81.124 v Velocity[Z] -19.135 378.62 25.68 1.9882 v ǁVelocityǁ 0.23036 701.9 260.64 83.863 v Pressure 48363 1.1024e+05 1.034e+05 1.0415e+05 v k 1.1753e-08 44790 917.96 355.37 v omega 154.84 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 80639 6.295e+05 3.4164e+05 2.4858e+05 v temperature 47.882 533.94 397.71 337.24 v Density 0.37819 5.9145 0.94864 1.0901 v TurbVisc 8.7515e-19 0.064078 0.01008 0.028659 v CourantNb 1.3009e-05 44.351 0.3989 0.0076118 v FourierNb 4.5363e-05 200.87 1.8143 0.090758 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 48.109 533.94 401.79 421.71 v Boundary Density 0.37832 5.8949 1.0024 0.9013 v Yplus 0 49.767 2.4677 0.97095 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8212e-05 44.899 0.48914 0.010644 INSTANT 0.159361813E-01 TIME STEP NUMBER 30263 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.727464256E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560757729E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122201726E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58548E+02 Friction velocity uk : 0.10334E+01 0.58548E+02 Dimensionless distance yplus : 0.20540E-01 0.49848E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14426E-01 0.12778E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60138E+03 2 0.23284E-06 0.13085E+03 0.27600E+03 c Velocity[X] 0.19908E+01 c Velocity[Y] 0.10889E+02 c Velocity[Z] 0.11797E+03 c Pressure 0.76320E-01 10 0.85515E-08 0.10672E+08 0.85991E+02 c k 0.25198E+04 2 0.37360E-06 0.50115E+06 0.35274E+04 c omega 0.81519E+09 1 0.43451E-08 0.36174E+12 0.44037E+02 c TotEner 0.24236E+06 1 0.12828E-05 0.13973E+08 0.40688E+02 c temperature 0.00000E+00 0 0.00000E+00 0.39786E+02 0.50877E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9321e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.07 230.07 0.0016709 0.001294 v Velocity[Y] -0.12982 701.9 250.59 81.125 v Velocity[Z] -19.134 378.8 25.687 1.9884 v ǁVelocityǁ 0.23039 701.9 260.64 83.863 v Pressure 48345 1.1024e+05 1.0339e+05 1.0415e+05 v k 1.1753e-08 44823 918.07 355.37 v omega 154.84 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 80470 6.295e+05 3.4164e+05 2.4858e+05 v temperature 47.652 533.94 397.7 337.24 v Density 0.37806 5.9343 0.94864 1.0901 v TurbVisc 8.7513e-19 0.064077 0.01008 0.02866 v CourantNb 1.3005e-05 44.36 0.39897 0.007612 v FourierNb 4.5367e-05 200.82 1.8141 0.090759 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 47.882 533.94 401.78 421.71 v Boundary Density 0.37819 5.9145 1.0026 0.90135 v Yplus 0 49.848 2.4681 0.97118 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8207e-05 44.907 0.48922 0.010644 INSTANT 0.159364443E-01 TIME STEP NUMBER 30264 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.728710429E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560759180E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122125089E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58552E+02 Friction velocity uk : 0.10334E+01 0.58552E+02 Dimensionless distance yplus : 0.20540E-01 0.49930E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14426E-01 0.12782E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60138E+03 2 0.23279E-06 0.13298E+03 0.27823E+03 c Velocity[X] 0.20374E+01 c Velocity[Y] 0.10860E+02 c Velocity[Z] 0.12009E+03 c Pressure 0.76324E-01 10 0.72900E-08 0.10914E+08 0.86961E+02 c k 0.25207E+04 2 0.37972E-06 0.51264E+06 0.35668E+04 c omega 0.81519E+09 1 0.39434E-08 0.28251E+12 0.38917E+02 c TotEner 0.24236E+06 1 0.12889E-05 0.14209E+08 0.41031E+02 c temperature 0.00000E+00 0 0.00000E+00 0.40589E+02 0.51388E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9316e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.1 230.1 0.0016661 0.0012962 v Velocity[Y] -0.12981 701.9 250.59 81.126 v Velocity[Z] -19.134 378.99 25.694 1.9887 v ǁVelocityǁ 0.23042 701.9 260.65 83.864 v Pressure 48326 1.1024e+05 1.0339e+05 1.0415e+05 v k 1.1753e-08 44857 918.18 355.37 v omega 154.85 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 80298 6.295e+05 3.4164e+05 2.4858e+05 v temperature 47.419 533.94 397.7 337.24 v Density 0.37793 5.9546 0.94863 1.0901 v TurbVisc 8.7511e-19 0.064077 0.010081 0.02866 v CourantNb 1.3001e-05 44.369 0.39905 0.0076122 v FourierNb 4.5371e-05 200.78 1.8139 0.09076 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 47.652 533.94 401.76 421.7 v Boundary Density 0.37806 5.9343 1.0029 0.9014 v Yplus 0 49.93 2.4685 0.97141 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8201e-05 44.914 0.48929 0.010645 INSTANT 0.159367074E-01 TIME STEP NUMBER 30265 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.729923972E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560760694E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.122046393E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58556E+02 Friction velocity uk : 0.10334E+01 0.58556E+02 Dimensionless distance yplus : 0.20540E-01 0.50014E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14426E-01 0.12786E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60138E+03 2 0.23273E-06 0.13519E+03 0.28053E+03 c Velocity[X] 0.20863E+01 c Velocity[Y] 0.10860E+02 c Velocity[Z] 0.12225E+03 c Pressure 0.76328E-01 10 0.80775E-08 0.11165E+08 0.87953E+02 c k 0.25216E+04 2 0.38605E-06 0.52459E+06 0.36073E+04 c omega 0.81519E+09 1 0.37860E-08 0.31690E+12 0.41217E+02 c TotEner 0.24236E+06 1 0.12953E-05 0.14462E+08 0.41394E+02 c temperature 0.00000E+00 0 0.00000E+00 0.41418E+02 0.51910E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9311e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.13 230.13 0.001661 0.0012984 v Velocity[Y] -0.12981 701.9 250.59 81.126 v Velocity[Z] -19.134 379.18 25.701 1.9889 v ǁVelocityǁ 0.23045 701.9 260.65 83.865 v Pressure 48308 1.1024e+05 1.0339e+05 1.0415e+05 v k 1.1752e-08 44891 918.29 355.37 v omega 154.85 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 80124 6.295e+05 3.4164e+05 2.4858e+05 v temperature 47.184 533.94 397.7 337.24 v Density 0.37779 5.9752 0.94863 1.0901 v TurbVisc 8.7509e-19 0.064077 0.010081 0.02866 v CourantNb 1.2997e-05 44.378 0.39912 0.0076123 v FourierNb 4.5375e-05 200.73 1.8138 0.090761 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 47.419 533.94 401.75 421.7 v Boundary Density 0.37793 5.9546 1.0031 0.90146 v Yplus 0 50.014 2.4688 0.97165 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8196e-05 44.921 0.48937 0.010645 INSTANT 0.159369705E-01 TIME STEP NUMBER 30266 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.731103835E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560762260E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121965574E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58560E+02 Friction velocity uk : 0.10334E+01 0.58560E+02 Dimensionless distance yplus : 0.20540E-01 0.50099E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14426E-01 0.12790E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60138E+03 2 0.23268E-06 0.13745E+03 0.28287E+03 c Velocity[X] 0.21379E+01 c Velocity[Y] 0.10854E+02 c Velocity[Z] 0.12446E+03 c Pressure 0.76332E-01 10 0.79385E-08 0.11424E+08 0.88968E+02 c k 0.25226E+04 2 0.39259E-06 0.53691E+06 0.36485E+04 c omega 0.81519E+09 1 0.33580E-08 0.25338E+12 0.36856E+02 c TotEner 0.24237E+06 1 0.13020E-05 0.14720E+08 0.41762E+02 c temperature 0.00000E+00 0 0.00000E+00 0.42270E+02 0.52440E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9306e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.15 230.15 0.0016558 0.0013005 v Velocity[Y] -0.12981 701.9 250.59 81.127 v Velocity[Z] -19.133 379.36 25.708 1.9891 v ǁVelocityǁ 0.23048 701.9 260.66 83.866 v Pressure 48289 1.1024e+05 1.0339e+05 1.0415e+05 v k 1.1752e-08 44926 918.4 355.37 v omega 154.86 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 79948 6.295e+05 3.4164e+05 2.4858e+05 v temperature 46.945 533.94 397.7 337.24 v Density 0.37766 5.9962 0.94863 1.0901 v TurbVisc 8.7507e-19 0.064076 0.010081 0.02866 v CourantNb 1.2993e-05 44.387 0.3992 0.0076125 v FourierNb 4.5379e-05 200.69 1.8136 0.090762 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 47.184 533.94 401.73 421.7 v Boundary Density 0.37779 5.9752 1.0033 0.90151 v Yplus 0 50.099 2.4692 0.97188 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.819e-05 44.929 0.48944 0.010645 INSTANT 0.159372335E-01 TIME STEP NUMBER 30267 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.732248987E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560763858E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121882570E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58564E+02 Friction velocity uk : 0.10334E+01 0.58564E+02 Dimensionless distance yplus : 0.20540E-01 0.50186E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14426E-01 0.12794E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60139E+03 2 0.23263E-06 0.13978E+03 0.28525E+03 c Velocity[X] 0.21923E+01 c Velocity[Y] 0.10855E+02 c Velocity[Z] 0.12673E+03 c Pressure 0.76337E-01 10 0.82367E-08 0.11692E+08 0.90007E+02 c k 0.25236E+04 2 0.39933E-06 0.54966E+06 0.36907E+04 c omega 0.81519E+09 1 0.35411E-08 0.26112E+12 0.37414E+02 c TotEner 0.24237E+06 1 0.13089E-05 0.14988E+08 0.42139E+02 c temperature 0.00000E+00 0 0.00000E+00 0.43146E+02 0.52981E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9302e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.18 230.18 0.0016505 0.0013026 v Velocity[Y] -0.12981 701.9 250.59 81.128 v Velocity[Z] -19.133 379.55 25.715 1.9894 v ǁVelocityǁ 0.23051 701.9 260.66 83.867 v Pressure 48271 1.1024e+05 1.0339e+05 1.0415e+05 v k 1.1752e-08 44960 918.52 355.37 v omega 154.86 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 79770 6.295e+05 3.4164e+05 2.4858e+05 v temperature 46.703 533.94 397.69 337.24 v Density 0.37753 6.0176 0.94862 1.0901 v TurbVisc 8.7505e-19 0.064076 0.010081 0.02866 v CourantNb 1.2989e-05 44.396 0.39927 0.0076126 v FourierNb 4.5383e-05 200.65 1.8134 0.090763 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 46.945 533.94 401.72 421.7 v Boundary Density 0.37766 5.9962 1.0036 0.90156 v Yplus 0 50.186 2.4696 0.97213 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8185e-05 44.936 0.48952 0.010645 INSTANT 0.159374966E-01 TIME STEP NUMBER 30268 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.733358430E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560765481E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121797312E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58568E+02 Friction velocity uk : 0.10334E+01 0.58568E+02 Dimensionless distance yplus : 0.20540E-01 0.50274E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14426E-01 0.12798E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60139E+03 2 0.23258E-06 0.14217E+03 0.28767E+03 c Velocity[X] 0.22496E+01 c Velocity[Y] 0.10865E+02 c Velocity[Z] 0.12906E+03 c Pressure 0.76341E-01 10 0.82918E-08 0.11970E+08 0.91071E+02 c k 0.25245E+04 2 0.40630E-06 0.56285E+06 0.37339E+04 c omega 0.81519E+09 1 0.38359E-08 0.33446E+12 0.42344E+02 c TotEner 0.24237E+06 1 0.13160E-05 0.15265E+08 0.42528E+02 c temperature 0.00000E+00 0 0.00000E+00 0.44047E+02 0.53532E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9297e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.21 230.21 0.0016451 0.0013047 v Velocity[Y] -0.12981 701.9 250.59 81.129 v Velocity[Z] -19.132 379.74 25.722 1.9896 v ǁVelocityǁ 0.23054 701.9 260.67 83.868 v Pressure 48252 1.1024e+05 1.0339e+05 1.0415e+05 v k 1.1752e-08 44996 918.64 355.37 v omega 154.87 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 79589 6.295e+05 3.4164e+05 2.4858e+05 v temperature 46.458 533.94 397.69 337.24 v Density 0.37739 6.0394 0.94862 1.0901 v TurbVisc 8.7503e-19 0.064076 0.010081 0.02866 v CourantNb 1.2985e-05 44.405 0.39935 0.0076128 v FourierNb 4.5388e-05 200.6 1.8132 0.090764 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 46.703 533.94 401.7 421.69 v Boundary Density 0.37753 6.0176 1.0038 0.90161 v Yplus 0 50.274 2.4701 0.97237 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8179e-05 44.944 0.48959 0.010646 INSTANT 0.159377597E-01 TIME STEP NUMBER 30269 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.734431200E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560767117E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121709731E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10334E+01 0.58572E+02 Friction velocity uk : 0.10334E+01 0.58572E+02 Dimensionless distance yplus : 0.20540E-01 0.50363E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14426E-01 0.12802E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60139E+03 2 0.23253E-06 0.14461E+03 0.29013E+03 c Velocity[X] 0.23101E+01 c Velocity[Y] 0.10865E+02 c Velocity[Z] 0.13144E+03 c Pressure 0.76345E-01 10 0.82003E-08 0.12259E+08 0.92161E+02 c k 0.25255E+04 2 0.41349E-06 0.57645E+06 0.37778E+04 c omega 0.81519E+09 1 0.35366E-08 0.29502E+12 0.39769E+02 c TotEner 0.24237E+06 1 0.13234E-05 0.15548E+08 0.42920E+02 c temperature 0.00000E+00 0 0.00000E+00 0.44974E+02 0.54092E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9292e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.24 230.24 0.0016396 0.0013067 v Velocity[Y] -0.12981 701.9 250.59 81.13 v Velocity[Z] -19.132 379.94 25.729 1.9898 v ǁVelocityǁ 0.23057 701.9 260.67 83.869 v Pressure 48233 1.1024e+05 1.0338e+05 1.0415e+05 v k 1.1751e-08 45031 918.75 355.37 v omega 154.87 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 79406 6.295e+05 3.4164e+05 2.4858e+05 v temperature 46.21 533.94 397.69 337.24 v Density 0.37726 6.0616 0.94862 1.0901 v TurbVisc 8.7501e-19 0.064075 0.010081 0.028661 v CourantNb 1.2981e-05 44.414 0.39943 0.0076129 v FourierNb 4.5392e-05 200.56 1.813 0.090766 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 46.458 533.94 401.68 421.69 v Boundary Density 0.37739 6.0394 1.0041 0.90167 v Yplus 0 50.363 2.4705 0.97262 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8174e-05 44.951 0.48967 0.010646 INSTANT 0.159380228E-01 TIME STEP NUMBER 30270 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.735466361E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560768762E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121619754E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58576E+02 Friction velocity uk : 0.10333E+01 0.58576E+02 Dimensionless distance yplus : 0.20540E-01 0.50455E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14426E-01 0.12807E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60139E+03 2 0.23249E-06 0.14712E+03 0.29263E+03 c Velocity[X] 0.23740E+01 c Velocity[Y] 0.10864E+02 c Velocity[Z] 0.13388E+03 c Pressure 0.76349E-01 10 0.85320E-08 0.12557E+08 0.93277E+02 c k 0.25265E+04 2 0.42091E-06 0.59049E+06 0.38226E+04 c omega 0.81519E+09 1 0.38174E-08 0.33792E+12 0.42563E+02 c TotEner 0.24237E+06 1 0.13311E-05 0.15839E+08 0.43319E+02 c temperature 0.00000E+00 0 0.00000E+00 0.45926E+02 0.54662E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9287e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.27 230.27 0.0016339 0.0013088 v Velocity[Y] -0.12981 701.9 250.59 81.131 v Velocity[Z] -19.131 380.13 25.736 1.9901 v ǁVelocityǁ 0.23059 701.9 260.68 83.87 v Pressure 48214 1.1024e+05 1.0338e+05 1.0415e+05 v k 1.1751e-08 45067 918.87 355.38 v omega 154.88 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 79220 6.295e+05 3.4164e+05 2.4858e+05 v temperature 45.959 533.94 397.68 337.24 v Density 0.37712 6.0843 0.94862 1.0901 v TurbVisc 8.7499e-19 0.064075 0.010081 0.028661 v CourantNb 1.2977e-05 44.423 0.3995 0.0076131 v FourierNb 4.5396e-05 200.52 1.8128 0.090767 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 46.21 533.94 401.67 421.69 v Boundary Density 0.37726 6.0616 1.0043 0.90173 v Yplus 0 50.455 2.4709 0.97288 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8168e-05 44.959 0.48974 0.010646 INSTANT 0.159382858E-01 TIME STEP NUMBER 30271 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.736463008E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560770412E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121527306E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58580E+02 Friction velocity uk : 0.10333E+01 0.58580E+02 Dimensionless distance yplus : 0.20540E-01 0.50548E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14426E-01 0.12811E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60140E+03 2 0.23244E-06 0.14969E+03 0.29517E+03 c Velocity[X] 0.24414E+01 c Velocity[Y] 0.10857E+02 c Velocity[Z] 0.13639E+03 c Pressure 0.76354E-01 10 0.85773E-08 0.12868E+08 0.94422E+02 c k 0.25276E+04 2 0.42858E-06 0.60501E+06 0.38683E+04 c omega 0.81519E+09 1 0.35746E-08 0.27066E+12 0.38092E+02 c TotEner 0.24237E+06 1 0.13390E-05 0.16138E+08 0.43726E+02 c temperature 0.00000E+00 0 0.00000E+00 0.46907E+02 0.55242E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9282e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.3 230.3 0.001628 0.0013108 v Velocity[Y] -0.12981 701.9 250.59 81.132 v Velocity[Z] -19.131 380.32 25.743 1.9903 v ǁVelocityǁ 0.23062 701.9 260.69 83.871 v Pressure 48195 1.1024e+05 1.0338e+05 1.0415e+05 v k 1.1751e-08 45103 918.99 355.38 v omega 154.88 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 79032 6.295e+05 3.4164e+05 2.4858e+05 v temperature 45.704 533.94 397.68 337.24 v Density 0.37699 6.1074 0.94861 1.0901 v TurbVisc 8.7497e-19 0.064074 0.010081 0.028661 v CourantNb 1.2973e-05 44.432 0.39958 0.0076132 v FourierNb 4.54e-05 200.47 1.8126 0.090768 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 45.959 533.94 401.65 421.68 v Boundary Density 0.37712 6.0843 1.0046 0.90178 v Yplus 0 50.548 2.4713 0.97313 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8162e-05 44.966 0.48982 0.010646 INSTANT 0.159385489E-01 TIME STEP NUMBER 30272 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.737420269E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560772060E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121432307E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58584E+02 Friction velocity uk : 0.10333E+01 0.58584E+02 Dimensionless distance yplus : 0.20539E-01 0.50642E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14426E-01 0.12815E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60140E+03 2 0.23240E-06 0.15233E+03 0.29777E+03 c Velocity[X] 0.25126E+01 c Velocity[Y] 0.10863E+02 c Velocity[Z] 0.13896E+03 c Pressure 0.76358E-01 10 0.95104E-08 0.13189E+08 0.95594E+02 c k 0.25286E+04 2 0.43651E-06 0.62007E+06 0.39152E+04 c omega 0.81519E+09 1 0.41617E-08 0.33117E+12 0.42135E+02 c TotEner 0.24237E+06 1 0.13472E-05 0.16447E+08 0.44144E+02 c temperature 0.00000E+00 0 0.00000E+00 0.47916E+02 0.55833E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9277e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.33 230.33 0.0016221 0.0013128 v Velocity[Y] -0.12981 701.9 250.59 81.133 v Velocity[Z] -19.13 380.52 25.751 1.9905 v ǁVelocityǁ 0.23065 701.9 260.69 83.872 v Pressure 48176 1.1024e+05 1.0338e+05 1.0415e+05 v k 1.1751e-08 45139 919.11 355.38 v omega 154.89 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 78842 6.295e+05 3.4164e+05 2.4858e+05 v temperature 45.446 533.94 397.68 337.24 v Density 0.37685 6.131 0.94861 1.0901 v TurbVisc 8.7495e-19 0.064074 0.010082 0.028661 v CourantNb 1.2968e-05 44.441 0.39966 0.0076134 v FourierNb 4.5405e-05 200.43 1.8124 0.090769 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 45.704 533.94 401.64 421.68 v Boundary Density 0.37699 6.1074 1.0049 0.90184 v Yplus 0 50.642 2.4718 0.97339 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8156e-05 44.974 0.4899 0.010646 INSTANT 0.159388120E-01 TIME STEP NUMBER 30273 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.738337300E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560773702E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121334676E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58589E+02 Friction velocity uk : 0.10333E+01 0.58589E+02 Dimensionless distance yplus : 0.20539E-01 0.50738E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14426E-01 0.12820E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60140E+03 2 0.23236E-06 0.15504E+03 0.30040E+03 c Velocity[X] 0.25879E+01 c Velocity[Y] 0.10858E+02 c Velocity[Z] 0.14159E+03 c Pressure 0.76362E-01 10 0.93706E-08 0.13523E+08 0.96798E+02 c k 0.25297E+04 2 0.44470E-06 0.63559E+06 0.39629E+04 c omega 0.81519E+09 1 0.43764E-08 0.35628E+12 0.43703E+02 c TotEner 0.24237E+06 1 0.13556E-05 0.16765E+08 0.44567E+02 c temperature 0.00000E+00 0 0.00000E+00 0.48955E+02 0.56435E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9272e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.36 230.36 0.001616 0.0013148 v Velocity[Y] -0.12981 701.9 250.59 81.134 v Velocity[Z] -19.13 380.72 25.758 1.9908 v ǁVelocityǁ 0.23067 701.9 260.7 83.873 v Pressure 48157 1.1024e+05 1.0338e+05 1.0415e+05 v k 1.175e-08 45176 919.24 355.38 v omega 154.89 9.6787e+09 1.8461e+08 3.4147e+05 v TotEner 78649 6.295e+05 3.4164e+05 2.4858e+05 v temperature 45.185 533.94 397.68 337.24 v Density 0.37671 6.1551 0.94861 1.0901 v TurbVisc 8.7493e-19 0.064074 0.010082 0.028661 v CourantNb 1.2964e-05 44.45 0.39973 0.0076136 v FourierNb 4.5409e-05 200.38 1.8122 0.09077 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 45.446 533.94 401.62 421.68 v Boundary Density 0.37685 6.131 1.0051 0.9019 v Yplus 0 50.738 2.4722 0.97366 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.815e-05 44.981 0.48997 0.010647 INSTANT 0.159390750E-01 TIME STEP NUMBER 30274 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.739213294E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560775352E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121234327E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58593E+02 Friction velocity uk : 0.10333E+01 0.58593E+02 Dimensionless distance yplus : 0.20539E-01 0.50836E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14425E-01 0.12824E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60141E+03 2 0.23232E-06 0.15783E+03 0.30309E+03 c Velocity[X] 0.26676E+01 c Velocity[Y] 0.10865E+02 c Velocity[Z] 0.14430E+03 c Pressure 0.76367E-01 11 0.63745E-08 0.13870E+08 0.98032E+02 c k 0.25307E+04 2 0.45317E-06 0.65167E+06 0.40117E+04 c omega 0.81519E+09 1 0.49361E-08 0.40747E+12 0.46738E+02 c TotEner 0.24238E+06 1 0.13644E-05 0.17094E+08 0.45003E+02 c temperature 0.00000E+00 0 0.00000E+00 0.50025E+02 0.57048E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9267e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.38 230.39 0.0016098 0.0013168 v Velocity[Y] -0.1298 701.9 250.59 81.135 v Velocity[Z] -19.129 380.91 25.765 1.991 v ǁVelocityǁ 0.2307 701.9 260.7 83.874 v Pressure 48138 1.1024e+05 1.0337e+05 1.0415e+05 v k 1.175e-08 45213 919.37 355.38 v omega 154.9 9.6787e+09 1.8462e+08 3.4147e+05 v TotEner 78453 6.295e+05 3.4164e+05 2.4858e+05 v temperature 44.92 533.94 397.67 337.24 v Density 0.37657 6.1797 0.9486 1.0901 v TurbVisc 8.7491e-19 0.064073 0.010082 0.028661 v CourantNb 1.296e-05 44.459 0.39981 0.0076137 v FourierNb 4.5414e-05 200.34 1.812 0.090771 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 45.185 533.94 401.6 421.67 v Boundary Density 0.37671 6.1551 1.0054 0.90196 v Yplus 0 50.836 2.4727 0.97393 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8144e-05 44.989 0.49005 0.010647 INSTANT 0.159393381E-01 TIME STEP NUMBER 30275 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.740047482E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560777016E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121131170E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58597E+02 Friction velocity uk : 0.10333E+01 0.58597E+02 Dimensionless distance yplus : 0.20539E-01 0.50936E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14425E-01 0.12829E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60141E+03 2 0.23228E-06 0.16068E+03 0.30581E+03 c Velocity[X] 0.27520E+01 c Velocity[Y] 0.10858E+02 c Velocity[Z] 0.14707E+03 c Pressure 0.76371E-01 10 0.98365E-08 0.14231E+08 0.99300E+02 c k 0.25318E+04 2 0.46193E-06 0.66827E+06 0.40614E+04 c omega 0.81519E+09 1 0.41324E-08 0.29445E+12 0.39731E+02 c TotEner 0.24238E+06 1 0.13735E-05 0.17430E+08 0.45443E+02 c temperature 0.00000E+00 0 0.00000E+00 0.51126E+02 0.57672E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9262e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.41 230.41 0.0016033 0.0013188 v Velocity[Y] -0.1298 701.9 250.59 81.136 v Velocity[Z] -19.129 381.11 25.773 1.9912 v ǁVelocityǁ 0.23073 701.9 260.71 83.875 v Pressure 48119 1.1024e+05 1.0337e+05 1.0415e+05 v k 1.175e-08 45250 919.49 355.38 v omega 154.9 9.6787e+09 1.8462e+08 3.4147e+05 v TotEner 78254 6.295e+05 3.4164e+05 2.4858e+05 v temperature 44.651 533.94 397.67 337.24 v Density 0.37644 6.2047 0.9486 1.0901 v TurbVisc 8.7489e-19 0.064073 0.010082 0.028662 v CourantNb 1.2955e-05 44.469 0.39989 0.0076139 v FourierNb 4.5418e-05 200.3 1.8118 0.090772 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 44.92 533.94 401.59 421.67 v Boundary Density 0.37657 6.1797 1.0057 0.90202 v Yplus 0 50.936 2.4732 0.97421 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8138e-05 44.996 0.49013 0.010647 INSTANT 0.159396012E-01 TIME STEP NUMBER 30276 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.740839129E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560778704E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.121025113E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58601E+02 Friction velocity uk : 0.10333E+01 0.58601E+02 Dimensionless distance yplus : 0.20539E-01 0.51038E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14425E-01 0.12834E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60141E+03 2 0.23225E-06 0.16363E+03 0.30859E+03 c Velocity[X] 0.28414E+01 c Velocity[Y] 0.10861E+02 c Velocity[Z] 0.14992E+03 c Pressure 0.76375E-01 10 0.98548E-08 0.14607E+08 0.10060E+03 c k 0.25329E+04 2 0.47101E-06 0.68550E+06 0.41123E+04 c omega 0.81519E+09 1 0.48897E-08 0.50048E+12 0.51798E+02 c TotEner 0.24238E+06 1 0.13829E-05 0.17780E+08 0.45896E+02 c temperature 0.00000E+00 0 0.00000E+00 0.52260E+02 0.58309E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9257e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.44 230.44 0.0015967 0.0013208 v Velocity[Y] -0.1298 701.9 250.59 81.137 v Velocity[Z] -19.129 381.31 25.78 1.9915 v ǁVelocityǁ 0.23075 701.9 260.71 83.876 v Pressure 48100 1.1024e+05 1.0337e+05 1.0415e+05 v k 1.175e-08 45288 919.62 355.38 v omega 154.91 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 78053 6.295e+05 3.4164e+05 2.4858e+05 v temperature 44.379 533.94 397.67 337.24 v Density 0.3763 6.2303 0.9486 1.0901 v TurbVisc 8.7488e-19 0.064073 0.010082 0.028662 v CourantNb 1.2951e-05 44.478 0.39997 0.007614 v FourierNb 4.5423e-05 200.25 1.8116 0.090773 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 44.651 533.94 401.57 421.67 v Boundary Density 0.37644 6.2047 1.006 0.90208 v Yplus 0 51.038 2.4736 0.97449 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8132e-05 45.004 0.49021 0.010647 INSTANT 0.159398643E-01 TIME STEP NUMBER 30277 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.741587539E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560780426E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.120916058E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58605E+02 Friction velocity uk : 0.10333E+01 0.58605E+02 Dimensionless distance yplus : 0.20539E-01 0.51141E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14425E-01 0.12839E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60142E+03 2 0.23222E-06 0.16667E+03 0.31145E+03 c Velocity[X] 0.29362E+01 c Velocity[Y] 0.10886E+02 c Velocity[Z] 0.15285E+03 c Pressure 0.76380E-01 10 0.97540E-08 0.14998E+08 0.10194E+03 c k 0.25340E+04 2 0.48040E-06 0.70339E+06 0.41645E+04 c omega 0.81519E+09 1 0.48386E-08 0.50068E+12 0.51808E+02 c TotEner 0.24238E+06 1 0.13928E-05 0.18145E+08 0.46366E+02 c temperature 0.00000E+00 0 0.00000E+00 0.53432E+02 0.58959E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9252e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.47 230.47 0.0015898 0.0013227 v Velocity[Y] -0.1298 701.9 250.59 81.138 v Velocity[Z] -19.128 381.51 25.788 1.9917 v ǁVelocityǁ 0.23078 701.9 260.72 83.877 v Pressure 48080 1.1024e+05 1.0337e+05 1.0415e+05 v k 1.1749e-08 45326 919.75 355.38 v omega 154.91 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 77849 6.295e+05 3.4164e+05 2.4859e+05 v temperature 44.103 533.94 397.66 337.24 v Density 0.37616 6.2565 0.9486 1.0901 v TurbVisc 8.7486e-19 0.064072 0.010082 0.028662 v CourantNb 1.2946e-05 44.487 0.40004 0.0076142 v FourierNb 4.5427e-05 200.21 1.8114 0.090774 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 44.379 533.94 401.55 421.66 v Boundary Density 0.3763 6.2303 1.0063 0.90215 v Yplus 0 51.141 2.4741 0.97477 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8126e-05 45.012 0.49029 0.010647 INSTANT 0.159401273E-01 TIME STEP NUMBER 30278 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.742292049E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560782185E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.120803905E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58609E+02 Friction velocity uk : 0.10333E+01 0.58609E+02 Dimensionless distance yplus : 0.20539E-01 0.51247E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14425E-01 0.12844E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60142E+03 2 0.23219E-06 0.16980E+03 0.31436E+03 c Velocity[X] 0.30368E+01 c Velocity[Y] 0.10907E+02 c Velocity[Z] 0.15585E+03 c Pressure 0.76384E-01 10 0.94493E-08 0.15405E+08 0.10331E+03 c k 0.25352E+04 2 0.49014E-06 0.72196E+06 0.42179E+04 c omega 0.81519E+09 1 0.44617E-08 0.41606E+12 0.47228E+02 c TotEner 0.24238E+06 1 0.14030E-05 0.18521E+08 0.46843E+02 c temperature 0.00000E+00 0 0.00000E+00 0.54638E+02 0.59620E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9247e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.5 230.5 0.0015827 0.0013247 v Velocity[Y] -0.1298 701.9 250.59 81.139 v Velocity[Z] -19.128 381.72 25.795 1.9919 v ǁVelocityǁ 0.2308 701.9 260.72 83.878 v Pressure 48061 1.1024e+05 1.0337e+05 1.0415e+05 v k 1.1749e-08 45364 919.88 355.38 v omega 154.92 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 77642 6.295e+05 3.4164e+05 2.4859e+05 v temperature 43.822 533.94 397.66 337.24 v Density 0.37602 6.2832 0.94859 1.0901 v TurbVisc 8.7484e-19 0.064072 0.010082 0.028662 v CourantNb 1.2942e-05 44.497 0.40012 0.0076144 v FourierNb 4.5432e-05 200.16 1.8112 0.090775 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 44.103 533.94 401.53 421.66 v Boundary Density 0.37616 6.2565 1.0066 0.90221 v Yplus 0 51.247 2.4746 0.97506 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.812e-05 45.019 0.49036 0.010648 INSTANT 0.159403904E-01 TIME STEP NUMBER 30279 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.742952037E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560783988E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.120688547E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58613E+02 Friction velocity uk : 0.10333E+01 0.58613E+02 Dimensionless distance yplus : 0.20539E-01 0.51355E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14425E-01 0.12849E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60142E+03 2 0.23216E-06 0.17300E+03 0.31730E+03 c Velocity[X] 0.31436E+01 c Velocity[Y] 0.10915E+02 c Velocity[Z] 0.15894E+03 c Pressure 0.76389E-01 10 0.87428E-08 0.15829E+08 0.10473E+03 c k 0.25363E+04 2 0.50022E-06 0.74114E+06 0.42724E+04 c omega 0.81519E+09 1 0.42550E-08 0.36338E+12 0.44137E+02 c TotEner 0.24238E+06 1 0.14135E-05 0.18906E+08 0.47327E+02 c temperature 0.00000E+00 0 0.00000E+00 0.55880E+02 0.60294E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9242e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.53 230.53 0.0015749 0.0013266 v Velocity[Y] -0.1298 701.9 250.59 81.14 v Velocity[Z] -19.127 381.92 25.803 1.9922 v ǁVelocityǁ 0.23083 701.9 260.73 83.879 v Pressure 48042 1.1024e+05 1.0336e+05 1.0415e+05 v k 1.1749e-08 45403 920.02 355.39 v omega 154.92 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 77432 6.295e+05 3.4164e+05 2.4859e+05 v temperature 43.538 533.94 397.66 337.24 v Density 0.37588 6.3105 0.94859 1.0901 v TurbVisc 8.7482e-19 0.064072 0.010083 0.028662 v CourantNb 1.2937e-05 44.506 0.4002 0.0076145 v FourierNb 4.5436e-05 200.12 1.811 0.090776 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 43.822 533.94 401.51 421.66 v Boundary Density 0.37602 6.2832 1.0069 0.90228 v Yplus 0 51.355 2.4751 0.97536 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8114e-05 45.027 0.49044 0.010648 INSTANT 0.159406535E-01 TIME STEP NUMBER 30280 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.743566919E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560785838E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.120569875E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58618E+02 Friction velocity uk : 0.10333E+01 0.58618E+02 Dimensionless distance yplus : 0.20539E-01 0.51464E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14425E-01 0.12854E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60142E+03 2 0.23214E-06 0.17630E+03 0.32031E+03 c Velocity[X] 0.32570E+01 c Velocity[Y] 0.10926E+02 c Velocity[Z] 0.16211E+03 c Pressure 0.76393E-01 10 0.87032E-08 0.16271E+08 0.10618E+03 c k 0.25375E+04 2 0.51066E-06 0.76102E+06 0.43281E+04 c omega 0.81519E+09 1 0.39519E-08 0.32359E+12 0.41650E+02 c TotEner 0.24238E+06 1 0.14243E-05 0.19303E+08 0.47822E+02 c temperature 0.00000E+00 0 0.00000E+00 0.57161E+02 0.60981E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9237e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.56 230.56 0.0015665 0.0013284 v Velocity[Y] -0.1298 701.9 250.59 81.141 v Velocity[Z] -19.127 382.13 25.811 1.9924 v ǁVelocityǁ 0.23085 701.9 260.73 83.88 v Pressure 48022 1.1024e+05 1.0336e+05 1.0415e+05 v k 1.1749e-08 45442 920.15 355.39 v omega 154.93 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 77219 6.295e+05 3.4164e+05 2.4859e+05 v temperature 43.25 533.94 397.65 337.24 v Density 0.37574 6.3384 0.94859 1.0901 v TurbVisc 8.748e-19 0.064071 0.010083 0.028662 v CourantNb 1.2933e-05 44.515 0.40028 0.0076147 v FourierNb 4.5441e-05 200.07 1.8108 0.090777 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 43.538 533.94 401.5 421.65 v Boundary Density 0.37588 6.3105 1.0072 0.90235 v Yplus 0 51.464 2.4756 0.97566 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8107e-05 45.035 0.49052 0.010648 INSTANT 0.159409166E-01 TIME STEP NUMBER 30281 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.744136150E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560787736E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.120447772E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58622E+02 Friction velocity uk : 0.10333E+01 0.58622E+02 Dimensionless distance yplus : 0.20539E-01 0.51576E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14425E-01 0.12859E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60143E+03 2 0.23212E-06 0.17965E+03 0.32333E+03 c Velocity[X] 0.33776E+01 c Velocity[Y] 0.10894E+02 c Velocity[Z] 0.16538E+03 c Pressure 0.76398E-01 10 0.85224E-08 0.16733E+08 0.10767E+03 c k 0.25387E+04 2 0.52148E-06 0.78152E+06 0.43848E+04 c omega 0.81519E+09 1 0.38936E-08 0.34005E+12 0.42696E+02 c TotEner 0.24239E+06 1 0.14356E-05 0.19701E+08 0.48313E+02 c temperature 0.00000E+00 0 0.00000E+00 0.58478E+02 0.61680E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9232e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.59 230.59 0.0015573 0.0013303 v Velocity[Y] -0.1298 701.9 250.6 81.141 v Velocity[Z] -19.126 382.33 25.818 1.9927 v ǁVelocityǁ 0.23088 701.9 260.74 83.881 v Pressure 48002 1.1024e+05 1.0336e+05 1.0415e+05 v k 1.1748e-08 45482 920.29 355.39 v omega 154.93 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 77002 6.295e+05 3.4164e+05 2.4859e+05 v temperature 42.957 533.94 397.65 337.24 v Density 0.37559 6.367 0.94859 1.09 v TurbVisc 8.7478e-19 0.064071 0.010083 0.028662 v CourantNb 1.2928e-05 44.525 0.40036 0.0076149 v FourierNb 4.5446e-05 200.03 1.8106 0.090779 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 43.25 533.94 401.48 421.65 v Boundary Density 0.37574 6.3384 1.0075 0.90241 v Yplus 0 51.576 2.4762 0.97596 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8101e-05 45.043 0.4906 0.010648 INSTANT 0.159411796E-01 TIME STEP NUMBER 30282 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.744659223E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560789682E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.120322118E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58626E+02 Friction velocity uk : 0.10333E+01 0.58626E+02 Dimensionless distance yplus : 0.20538E-01 0.51691E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14425E-01 0.12864E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60143E+03 2 0.23210E-06 0.18311E+03 0.32643E+03 c Velocity[X] 0.35059E+01 c Velocity[Y] 0.10875E+02 c Velocity[Z] 0.16873E+03 c Pressure 0.76402E-01 10 0.87379E-08 0.17215E+08 0.10921E+03 c k 0.25399E+04 2 0.53271E-06 0.80287E+06 0.44430E+04 c omega 0.81519E+09 1 0.37256E-08 0.28480E+12 0.39074E+02 c TotEner 0.24239E+06 1 0.14473E-05 0.20118E+08 0.48820E+02 c temperature 0.00000E+00 0 0.00000E+00 0.59839E+02 0.62393E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9227e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.62 230.62 0.0015475 0.0013321 v Velocity[Y] -0.1298 701.9 250.6 81.142 v Velocity[Z] -19.126 382.54 25.826 1.9929 v ǁVelocityǁ 0.2309 701.9 260.75 83.881 v Pressure 47983 1.1024e+05 1.0336e+05 1.0415e+05 v k 1.1748e-08 45521 920.43 355.39 v omega 154.94 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 76783 6.295e+05 3.4164e+05 2.4859e+05 v temperature 42.661 533.94 397.65 337.24 v Density 0.37545 6.3962 0.94858 1.09 v TurbVisc 8.7476e-19 0.06407 0.010083 0.028663 v CourantNb 1.2923e-05 44.534 0.40044 0.007615 v FourierNb 4.545e-05 199.99 1.8104 0.09078 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 42.957 533.94 401.46 421.64 v Boundary Density 0.37559 6.367 1.0078 0.90248 v Yplus 0 51.691 2.4767 0.97627 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8094e-05 45.05 0.49068 0.010649 INSTANT 0.159414427E-01 TIME STEP NUMBER 30283 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.745135675E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560791668E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.120192787E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58630E+02 Friction velocity uk : 0.10333E+01 0.58630E+02 Dimensionless distance yplus : 0.20538E-01 0.51807E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14425E-01 0.12870E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60143E+03 2 0.23209E-06 0.18669E+03 0.32961E+03 c Velocity[X] 0.36426E+01 c Velocity[Y] 0.10871E+02 c Velocity[Z] 0.17218E+03 c Pressure 0.76407E-01 10 0.93107E-08 0.17718E+08 0.11080E+03 c k 0.25411E+04 2 0.54436E-06 0.82510E+06 0.45028E+04 c omega 0.81520E+09 1 0.38995E-08 0.34608E+12 0.43073E+02 c TotEner 0.24239E+06 1 0.14594E-05 0.20551E+08 0.49343E+02 c temperature 0.00000E+00 0 0.00000E+00 0.61243E+02 0.63121E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9222e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.65 230.65 0.0015372 0.0013339 v Velocity[Y] -0.1298 701.9 250.6 81.143 v Velocity[Z] -19.125 382.75 25.834 1.9932 v ǁVelocityǁ 0.23093 701.9 260.75 83.882 v Pressure 47963 1.1024e+05 1.0335e+05 1.0415e+05 v k 1.1748e-08 45562 920.57 355.39 v omega 154.94 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 76560 6.295e+05 3.4164e+05 2.4859e+05 v temperature 42.359 533.94 397.64 337.24 v Density 0.37531 6.426 0.94858 1.09 v TurbVisc 8.7474e-19 0.06407 0.010083 0.028663 v CourantNb 1.2919e-05 44.544 0.40052 0.0076152 v FourierNb 4.5455e-05 199.94 1.8102 0.090781 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 42.661 533.94 401.44 421.64 v Boundary Density 0.37545 6.3962 1.0081 0.90256 v Yplus 0 51.807 2.4773 0.97659 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8088e-05 45.058 0.49076 0.010649 INSTANT 0.159417058E-01 TIME STEP NUMBER 30284 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.745565081E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560793686E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.120059647E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58634E+02 Friction velocity uk : 0.10333E+01 0.58634E+02 Dimensionless distance yplus : 0.20538E-01 0.51926E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14425E-01 0.12875E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60144E+03 2 0.23208E-06 0.19038E+03 0.33284E+03 c Velocity[X] 0.37884E+01 c Velocity[Y] 0.10867E+02 c Velocity[Z] 0.17573E+03 c Pressure 0.76411E-01 10 0.88810E-08 0.18245E+08 0.11243E+03 c k 0.25424E+04 2 0.55647E-06 0.84822E+06 0.45641E+04 c omega 0.81520E+09 1 0.41523E-08 0.35594E+12 0.43682E+02 c TotEner 0.24239E+06 1 0.14721E-05 0.21000E+08 0.49879E+02 c temperature 0.00000E+00 0 0.00000E+00 0.62693E+02 0.63864E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9217e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.68 230.68 0.0015262 0.0013357 v Velocity[Y] -0.1298 701.9 250.6 81.144 v Velocity[Z] -19.125 382.96 25.842 1.9934 v ǁVelocityǁ 0.23095 701.9 260.76 83.883 v Pressure 47943 1.1024e+05 1.0335e+05 1.0415e+05 v k 1.1748e-08 45602 920.72 355.39 v omega 154.95 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 76334 6.295e+05 3.4164e+05 2.4859e+05 v temperature 42.053 533.94 397.64 337.24 v Density 0.37517 6.4566 0.94858 1.09 v TurbVisc 8.7473e-19 0.06407 0.010083 0.028663 v CourantNb 1.2914e-05 44.553 0.4006 0.0076154 v FourierNb 4.546e-05 199.9 1.81 0.090782 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 42.359 533.94 401.42 421.64 v Boundary Density 0.37531 6.426 1.0084 0.90263 v Yplus 0 51.926 2.4778 0.97691 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8081e-05 45.066 0.49084 0.010649 INSTANT 0.159419689E-01 TIME STEP NUMBER 30285 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.745947056E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560795719E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.119922560E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58639E+02 Friction velocity uk : 0.10333E+01 0.58639E+02 Dimensionless distance yplus : 0.20538E-01 0.52047E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14425E-01 0.12881E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60144E+03 2 0.23207E-06 0.19419E+03 0.33615E+03 c Velocity[X] 0.39440E+01 c Velocity[Y] 0.10864E+02 c Velocity[Z] 0.17938E+03 c Pressure 0.76416E-01 10 0.86705E-08 0.18796E+08 0.11412E+03 c k 0.25436E+04 2 0.56904E-06 0.87224E+06 0.46268E+04 c omega 0.81520E+09 1 0.40082E-08 0.33010E+12 0.42067E+02 c TotEner 0.24239E+06 1 0.14852E-05 0.21462E+08 0.50425E+02 c temperature 0.00000E+00 0 0.00000E+00 0.64190E+02 0.64622E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9212e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.71 230.71 0.0015144 0.0013375 v Velocity[Y] -0.1298 701.9 250.6 81.145 v Velocity[Z] -19.124 383.17 25.85 1.9936 v ǁVelocityǁ 0.23098 701.9 260.76 83.884 v Pressure 47923 1.1024e+05 1.0335e+05 1.0415e+05 v k 1.1747e-08 45643 920.87 355.4 v omega 154.95 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 76104 6.295e+05 3.4164e+05 2.4859e+05 v temperature 41.743 533.94 397.64 337.24 v Density 0.37502 6.4878 0.94858 1.09 v TurbVisc 8.7471e-19 0.064069 0.010083 0.028663 v CourantNb 1.2909e-05 44.563 0.40068 0.0076155 v FourierNb 4.5464e-05 199.85 1.8098 0.090783 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 42.053 533.94 401.4 421.63 v Boundary Density 0.37517 6.4566 1.0088 0.9027 v Yplus 0 52.047 2.4784 0.97724 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8074e-05 45.074 0.49092 0.010649 INSTANT 0.159422320E-01 TIME STEP NUMBER 30286 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.746281258E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560797743E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.119781382E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58643E+02 Friction velocity uk : 0.10333E+01 0.58643E+02 Dimensionless distance yplus : 0.20538E-01 0.52171E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14425E-01 0.12886E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60144E+03 2 0.23207E-06 0.19812E+03 0.33953E+03 c Velocity[X] 0.41101E+01 c Velocity[Y] 0.10869E+02 c Velocity[Z] 0.18314E+03 c Pressure 0.76421E-01 10 0.89113E-08 0.19374E+08 0.11586E+03 c k 0.25449E+04 2 0.58211E-06 0.89726E+06 0.46913E+04 c omega 0.81520E+09 1 0.35697E-08 0.27146E+12 0.38148E+02 c TotEner 0.24239E+06 1 0.14988E-05 0.21942E+08 0.50986E+02 c temperature 0.00000E+00 0 0.00000E+00 0.65737E+02 0.65395E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9207e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.74 230.74 0.0015017 0.0013392 v Velocity[Y] -0.1298 701.9 250.6 81.146 v Velocity[Z] -19.124 383.38 25.858 1.9939 v ǁVelocityǁ 0.231 701.9 260.77 83.885 v Pressure 47903 1.1024e+05 1.0335e+05 1.0415e+05 v k 1.1747e-08 45685 921.02 355.4 v omega 154.96 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 75870 6.295e+05 3.4164e+05 2.4859e+05 v temperature 41.427 533.94 397.63 337.25 v Density 0.37488 6.5199 0.94858 1.09 v TurbVisc 8.7469e-19 0.064069 0.010084 0.028663 v CourantNb 1.2904e-05 44.572 0.40077 0.0076157 v FourierNb 4.5469e-05 199.81 1.8096 0.090784 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 41.743 533.94 401.38 421.63 v Boundary Density 0.37502 6.4878 1.0091 0.90278 v Yplus 0 52.171 2.479 0.97757 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8068e-05 45.082 0.491 0.010649 INSTANT 0.159424950E-01 TIME STEP NUMBER 30287 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.746567391E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560799741E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.119635961E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58647E+02 Friction velocity uk : 0.10333E+01 0.58647E+02 Dimensionless distance yplus : 0.20538E-01 0.52298E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14425E-01 0.12892E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60145E+03 2 0.23207E-06 0.20216E+03 0.34298E+03 c Velocity[X] 0.42877E+01 c Velocity[Y] 0.10865E+02 c Velocity[Z] 0.18701E+03 c Pressure 0.76425E-01 10 0.89276E-08 0.19979E+08 0.11766E+03 c k 0.25462E+04 2 0.59569E-06 0.92327E+06 0.47573E+04 c omega 0.81520E+09 1 0.35274E-08 0.31710E+12 0.41230E+02 c TotEner 0.24239E+06 1 0.15130E-05 0.22437E+08 0.51557E+02 c temperature 0.00000E+00 0 0.00000E+00 0.67333E+02 0.66185E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9202e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.77 230.77 0.0014884 0.0013409 v Velocity[Y] -0.1298 701.9 250.6 81.147 v Velocity[Z] -19.124 383.6 25.866 1.9941 v ǁVelocityǁ 0.23102 701.9 260.78 83.886 v Pressure 47883 1.1024e+05 1.0335e+05 1.0415e+05 v k 1.1747e-08 45726 921.17 355.4 v omega 154.96 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 75633 6.295e+05 3.4164e+05 2.4859e+05 v temperature 41.107 533.94 397.63 337.25 v Density 0.37473 6.5527 0.94857 1.09 v TurbVisc 8.7467e-19 0.064069 0.010084 0.028663 v CourantNb 1.2899e-05 44.582 0.40085 0.0076159 v FourierNb 4.5474e-05 199.76 1.8094 0.090785 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 41.427 533.94 401.36 421.63 v Boundary Density 0.37488 6.5199 1.0095 0.90286 v Yplus 0 52.298 2.4796 0.97791 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8061e-05 45.09 0.49109 0.01065 INSTANT 0.159427581E-01 TIME STEP NUMBER 30288 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.746805198E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560801695E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.119486138E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58652E+02 Friction velocity uk : 0.10333E+01 0.58652E+02 Dimensionless distance yplus : 0.20538E-01 0.52427E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14425E-01 0.12898E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60145E+03 2 0.23208E-06 0.20634E+03 0.34650E+03 c Velocity[X] 0.44777E+01 c Velocity[Y] 0.10861E+02 c Velocity[Z] 0.19100E+03 c Pressure 0.76430E-01 10 0.91211E-08 0.20614E+08 0.11951E+03 c k 0.25476E+04 2 0.60983E-06 0.95035E+06 0.48251E+04 c omega 0.81520E+09 1 0.35832E-08 0.27706E+12 0.38540E+02 c TotEner 0.24240E+06 1 0.15277E-05 0.22948E+08 0.52141E+02 c temperature 0.00000E+00 0 0.00000E+00 0.68983E+02 0.66991E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9197e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.8 230.8 0.0014743 0.0013426 v Velocity[Y] -0.1298 701.9 250.6 81.148 v Velocity[Z] -19.123 383.81 25.874 1.9944 v ǁVelocityǁ 0.23105 701.9 260.78 83.887 v Pressure 47862 1.1024e+05 1.0334e+05 1.0415e+05 v k 1.1747e-08 45769 921.32 355.4 v omega 154.97 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 75392 6.295e+05 3.4164e+05 2.4859e+05 v temperature 40.781 533.94 397.63 337.25 v Density 0.37459 6.5863 0.94857 1.09 v TurbVisc 8.7465e-19 0.064068 0.010084 0.028664 v CourantNb 1.2894e-05 44.592 0.40093 0.007616 v FourierNb 4.5479e-05 199.72 1.8092 0.090786 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 41.107 533.94 401.34 421.62 v Boundary Density 0.37473 6.5527 1.0098 0.90294 v Yplus 0 52.427 2.4802 0.97826 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8054e-05 45.098 0.49117 0.01065 INSTANT 0.159430212E-01 TIME STEP NUMBER 30289 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.746994466E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560803586E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.119331746E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58656E+02 Friction velocity uk : 0.10333E+01 0.58656E+02 Dimensionless distance yplus : 0.20538E-01 0.52559E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.12904E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60145E+03 2 0.23209E-06 0.21065E+03 0.35010E+03 c Velocity[X] 0.46813E+01 c Velocity[Y] 0.10861E+02 c Velocity[Z] 0.19511E+03 c Pressure 0.76435E-01 10 0.93106E-08 0.21281E+08 0.12143E+03 c k 0.25489E+04 2 0.62454E-06 0.97858E+06 0.48947E+04 c omega 0.81520E+09 1 0.35609E-08 0.29128E+12 0.39516E+02 c TotEner 0.24240E+06 1 0.15430E-05 0.23479E+08 0.52740E+02 c temperature 0.00000E+00 0 0.00000E+00 0.70689E+02 0.67814E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9191e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.83 230.84 0.0014596 0.0013443 v Velocity[Y] -0.12979 701.9 250.6 81.149 v Velocity[Z] -19.123 384.03 25.882 1.9946 v ǁVelocityǁ 0.23107 701.9 260.79 83.888 v Pressure 47842 1.1024e+05 1.0334e+05 1.0415e+05 v k 1.1746e-08 45811 921.48 355.4 v omega 154.97 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 75148 6.295e+05 3.4164e+05 2.4859e+05 v temperature 40.451 533.94 397.62 337.25 v Density 0.37444 6.6207 0.94857 1.09 v TurbVisc 8.7463e-19 0.064068 0.010084 0.028664 v CourantNb 1.2889e-05 44.601 0.40101 0.0076162 v FourierNb 4.5484e-05 199.67 1.809 0.090788 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 40.781 533.94 401.32 421.62 v Boundary Density 0.37459 6.5863 1.0102 0.90302 v Yplus 0 52.559 2.4809 0.97861 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8047e-05 45.106 0.49125 0.01065 INSTANT 0.159432843E-01 TIME STEP NUMBER 30290 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.747135028E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560805407E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.119172611E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58660E+02 Friction velocity uk : 0.10333E+01 0.58660E+02 Dimensionless distance yplus : 0.20538E-01 0.52695E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.12910E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60146E+03 2 0.23211E-06 0.21508E+03 0.35376E+03 c Velocity[X] 0.48977E+01 c Velocity[Y] 0.10857E+02 c Velocity[Z] 0.19933E+03 c Pressure 0.76439E-01 10 0.97346E-08 0.21982E+08 0.12341E+03 c k 0.25503E+04 2 0.63987E-06 0.10019E+07 0.49511E+04 c omega 0.81520E+09 1 0.34696E-08 0.25256E+12 0.36796E+02 c TotEner 0.24240E+06 1 0.15589E-05 0.24021E+08 0.53346E+02 c temperature 0.00000E+00 0 0.00000E+00 0.72462E+02 0.68659E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9186e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.86 230.87 0.0014441 0.001346 v Velocity[Y] -0.12979 701.9 250.6 81.15 v Velocity[Z] -19.122 384.25 25.891 1.9949 v ǁVelocityǁ 0.23109 701.9 260.79 83.889 v Pressure 47822 1.1024e+05 1.0334e+05 1.0415e+05 v k 1.1746e-08 45854 921.64 355.4 v omega 154.98 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 74899 6.295e+05 3.4164e+05 2.4859e+05 v temperature 40.114 533.94 397.62 337.25 v Density 0.37429 6.6561 0.94857 1.09 v TurbVisc 8.7461e-19 0.064068 0.010084 0.028664 v CourantNb 1.2884e-05 44.611 0.40109 0.0076164 v FourierNb 4.5489e-05 199.63 1.8088 0.090789 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 40.451 533.94 401.3 421.61 v Boundary Density 0.37444 6.6207 1.0105 0.9031 v Yplus 0 52.695 2.4815 0.97897 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.804e-05 45.114 0.49133 0.01065 INSTANT 0.159435474E-01 TIME STEP NUMBER 30291 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.747226757E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560807156E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.119008550E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10333E+01 0.58665E+02 Friction velocity uk : 0.10333E+01 0.58665E+02 Dimensionless distance yplus : 0.20538E-01 0.52833E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.12916E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60146E+03 2 0.23214E-06 0.21969E+03 0.35752E+03 c Velocity[X] 0.51312E+01 c Velocity[Y] 0.10862E+02 c Velocity[Z] 0.20370E+03 c Pressure 0.76444E-01 11 0.74950E-08 0.22719E+08 0.12547E+03 c k 0.25517E+04 2 0.65584E-06 0.10364E+07 0.50340E+04 c omega 0.81520E+09 1 0.32849E-08 0.21339E+12 0.33823E+02 c TotEner 0.24240E+06 1 0.15755E-05 0.24591E+08 0.53975E+02 c temperature 0.00000E+00 0 0.00000E+00 0.74275E+02 0.69512E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9181e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.9 230.9 0.0014278 0.0013476 v Velocity[Y] -0.12979 701.9 250.6 81.151 v Velocity[Z] -19.122 384.47 25.899 1.9951 v ǁVelocityǁ 0.23112 701.9 260.8 83.89 v Pressure 47801 1.1024e+05 1.0334e+05 1.0415e+05 v k 1.1746e-08 45897 921.81 355.41 v omega 154.98 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 74646 6.295e+05 3.4164e+05 2.4859e+05 v temperature 39.773 533.94 397.62 337.25 v Density 0.37414 6.6923 0.94857 1.09 v TurbVisc 8.7459e-19 0.064067 0.010084 0.028664 v CourantNb 1.2879e-05 44.621 0.40118 0.0076165 v FourierNb 4.5494e-05 199.58 1.8085 0.09079 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 40.114 533.94 401.28 421.61 v Boundary Density 0.37429 6.6561 1.0109 0.90319 v Yplus 0 52.833 2.4822 0.97934 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8033e-05 45.122 0.49142 0.010651 INSTANT 0.159438104E-01 TIME STEP NUMBER 30292 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.747269572E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560808834E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.118839368E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58669E+02 Friction velocity uk : 0.10332E+01 0.58669E+02 Dimensionless distance yplus : 0.20538E-01 0.52974E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.12923E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60146E+03 2 0.23217E-06 0.22444E+03 0.36137E+03 c Velocity[X] 0.53805E+01 c Velocity[Y] 0.10876E+02 c Velocity[Z] 0.20818E+03 c Pressure 0.76449E-01 11 0.70066E-08 0.23495E+08 0.12759E+03 c k 0.25532E+04 2 0.67250E-06 0.10646E+07 0.51003E+04 c omega 0.81520E+09 1 0.40045E-08 0.34780E+12 0.43180E+02 c TotEner 0.24240E+06 1 0.15927E-05 0.25178E+08 0.54615E+02 c temperature 0.00000E+00 0 0.00000E+00 0.76170E+02 0.70394E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9176e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.93 230.93 0.0014107 0.0013492 v Velocity[Y] -0.12979 701.9 250.6 81.152 v Velocity[Z] -19.121 384.69 25.907 1.9954 v ǁVelocityǁ 0.23114 701.9 260.81 83.891 v Pressure 47781 1.1024e+05 1.0333e+05 1.0415e+05 v k 1.1746e-08 45941 921.98 355.41 v omega 154.99 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 74388 6.295e+05 3.4164e+05 2.4859e+05 v temperature 39.425 533.94 397.61 337.25 v Density 0.374 6.7295 0.94857 1.09 v TurbVisc 8.7458e-19 0.064067 0.010084 0.028664 v CourantNb 1.2874e-05 44.631 0.40126 0.0076167 v FourierNb 4.5499e-05 199.54 1.8083 0.090791 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 39.773 533.94 401.26 421.61 v Boundary Density 0.37414 6.6923 1.0113 0.90328 v Yplus 0 52.974 2.4829 0.97972 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8026e-05 45.13 0.4915 0.010651 INSTANT 0.159440735E-01 TIME STEP NUMBER 30293 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.747263437E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560810453E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.118664865E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58673E+02 Friction velocity uk : 0.10332E+01 0.58673E+02 Dimensionless distance yplus : 0.20537E-01 0.53119E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.12929E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60147E+03 2 0.23221E-06 0.22937E+03 0.36531E+03 c Velocity[X] 0.56506E+01 c Velocity[Y] 0.10876E+02 c Velocity[Z] 0.21284E+03 c Pressure 0.76454E-01 10 0.96783E-08 0.24314E+08 0.12980E+03 c k 0.25546E+04 2 0.68987E-06 0.11032E+07 0.51901E+04 c omega 0.81520E+09 1 0.34266E-08 0.25003E+12 0.36611E+02 c TotEner 0.24240E+06 1 0.16106E-05 0.25788E+08 0.55273E+02 c temperature 0.00000E+00 0 0.00000E+00 0.78112E+02 0.71285E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.917e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.96 230.96 0.001393 0.0013508 v Velocity[Y] -0.12979 701.9 250.6 81.153 v Velocity[Z] -19.121 384.91 25.916 1.9956 v ǁVelocityǁ 0.23116 701.9 260.81 83.892 v Pressure 47760 1.1024e+05 1.0333e+05 1.0415e+05 v k 1.1745e-08 45985 922.14 355.41 v omega 154.99 9.6787e+09 1.8462e+08 3.4148e+05 v TotEner 74127 6.295e+05 3.4164e+05 2.4859e+05 v temperature 39.072 533.94 397.61 337.25 v Density 0.37385 6.7677 0.94856 1.09 v TurbVisc 8.7456e-19 0.064066 0.010085 0.028664 v CourantNb 1.2868e-05 44.64 0.40135 0.0076169 v FourierNb 4.5504e-05 199.49 1.8081 0.090792 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 39.425 533.94 401.24 421.6 v Boundary Density 0.374 6.7295 1.0117 0.90337 v Yplus 0 53.119 2.4835 0.9801 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8018e-05 45.138 0.49158 0.010651 INSTANT 0.159443366E-01 TIME STEP NUMBER 30294 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.747208357E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560812027E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.118484825E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58678E+02 Friction velocity uk : 0.10332E+01 0.58678E+02 Dimensionless distance yplus : 0.20537E-01 0.53267E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.12936E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60147E+03 2 0.23226E-06 0.23444E+03 0.36932E+03 c Velocity[X] 0.59398E+01 c Velocity[Y] 0.10874E+02 c Velocity[Z] 0.21762E+03 c Pressure 0.76459E-01 10 0.91061E-08 0.25178E+08 0.13208E+03 c k 0.25561E+04 2 0.70801E-06 0.11341E+07 0.52604E+04 c omega 0.81520E+09 1 0.44888E-08 0.47085E+12 0.50241E+02 c TotEner 0.24240E+06 1 0.16293E-05 0.26414E+08 0.55939E+02 c temperature 0.00000E+00 0 0.00000E+00 0.80141E+02 0.72205E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9165e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -230.99 230.99 0.0013745 0.0013524 v Velocity[Y] -0.12979 701.9 250.6 81.154 v Velocity[Z] -19.12 385.13 25.924 1.9959 v ǁVelocityǁ 0.23118 701.9 260.82 83.893 v Pressure 47739 1.1024e+05 1.0333e+05 1.0415e+05 v k 1.1745e-08 46029 922.32 355.41 v omega 155 9.6788e+09 1.8462e+08 3.4148e+05 v TotEner 73860 6.295e+05 3.4164e+05 2.4859e+05 v temperature 38.712 533.94 397.61 337.25 v Density 0.3737 6.8069 0.94856 1.09 v TurbVisc 8.7454e-19 0.064066 0.010085 0.028665 v CourantNb 1.2863e-05 44.65 0.40143 0.0076171 v FourierNb 4.5509e-05 199.45 1.8079 0.090793 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 39.072 533.94 401.22 421.6 v Boundary Density 0.37385 6.7677 1.0121 0.90346 v Yplus 0 53.267 2.4843 0.98049 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8011e-05 45.146 0.49167 0.010651 INSTANT 0.159445997E-01 TIME STEP NUMBER 30295 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.747104386E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560813556E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.118299026E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58682E+02 Friction velocity uk : 0.10332E+01 0.58682E+02 Dimensionless distance yplus : 0.20537E-01 0.53419E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.12942E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60147E+03 2 0.23232E-06 0.23971E+03 0.37344E+03 c Velocity[X] 0.62532E+01 c Velocity[Y] 0.10873E+02 c Velocity[Z] 0.22258E+03 c Pressure 0.76464E-01 10 0.90271E-08 0.26090E+08 0.13445E+03 c k 0.25576E+04 2 0.72696E-06 0.11740E+07 0.53504E+04 c omega 0.81520E+09 1 0.46011E-08 0.41114E+12 0.46947E+02 c TotEner 0.24241E+06 1 0.16488E-05 0.27068E+08 0.56627E+02 c temperature 0.00000E+00 0 0.00000E+00 0.82230E+02 0.73140E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.916e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.02 231.02 0.0013553 0.001354 v Velocity[Y] -0.12979 701.9 250.6 81.155 v Velocity[Z] -19.12 385.36 25.933 1.9961 v ǁVelocityǁ 0.23121 701.9 260.83 83.894 v Pressure 47718 1.1024e+05 1.0333e+05 1.0415e+05 v k 1.1745e-08 46075 922.49 355.42 v omega 155 9.6788e+09 1.8462e+08 3.4148e+05 v TotEner 73589 6.295e+05 3.4164e+05 2.4859e+05 v temperature 38.346 533.94 397.6 337.25 v Density 0.37355 6.8471 0.94856 1.09 v TurbVisc 8.7452e-19 0.064066 0.010085 0.028665 v CourantNb 1.2858e-05 44.66 0.40151 0.0076172 v FourierNb 4.5514e-05 199.4 1.8077 0.090794 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 38.712 533.94 401.2 421.59 v Boundary Density 0.3737 6.8069 1.0125 0.90355 v Yplus 0 53.419 2.485 0.98089 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.8004e-05 45.154 0.49175 0.010652 INSTANT 0.159448628E-01 TIME STEP NUMBER 30296 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.746951619E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560815046E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.118107229E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58687E+02 Friction velocity uk : 0.10332E+01 0.58687E+02 Dimensionless distance yplus : 0.20537E-01 0.53574E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.12949E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60148E+03 2 0.23238E-06 0.24517E+03 0.37767E+03 c Velocity[X] 0.65914E+01 c Velocity[Y] 0.10877E+02 c Velocity[Z] 0.22771E+03 c Pressure 0.76469E-01 10 0.96204E-08 0.27056E+08 0.13692E+03 c k 0.25592E+04 2 0.74677E-06 0.12122E+07 0.54348E+04 c omega 0.81520E+09 1 0.48917E-08 0.51780E+12 0.52686E+02 c TotEner 0.24241E+06 1 0.16691E-05 0.27745E+08 0.57331E+02 c temperature 0.00000E+00 0 0.00000E+00 0.84400E+02 0.74099E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9155e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.05 231.05 0.0013354 0.0013555 v Velocity[Y] -0.12979 701.9 250.6 81.156 v Velocity[Z] -19.12 385.58 25.941 1.9964 v ǁVelocityǁ 0.23123 701.9 260.83 83.895 v Pressure 47697 1.1024e+05 1.0332e+05 1.0415e+05 v k 1.1745e-08 46120 922.67 355.42 v omega 155.01 9.6788e+09 1.8462e+08 3.4148e+05 v TotEner 73313 6.295e+05 3.4164e+05 2.4859e+05 v temperature 37.974 533.94 397.6 337.25 v Density 0.37339 6.8885 0.94856 1.09 v TurbVisc 8.745e-19 0.064065 0.010085 0.028665 v CourantNb 1.2852e-05 44.67 0.4016 0.0076174 v FourierNb 4.5519e-05 199.36 1.8075 0.090795 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 38.346 533.94 401.17 421.59 v Boundary Density 0.37355 6.8471 1.0129 0.90365 v Yplus 0 53.574 2.4857 0.9813 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7996e-05 45.163 0.49184 0.010652 INSTANT 0.159451259E-01 TIME STEP NUMBER 30297 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.746750197E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560816509E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.117909186E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58691E+02 Friction velocity uk : 0.10332E+01 0.58691E+02 Dimensionless distance yplus : 0.20537E-01 0.53733E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.12956E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60148E+03 2 0.23246E-06 0.25083E+03 0.38200E+03 c Velocity[X] 0.69566E+01 c Velocity[Y] 0.10881E+02 c Velocity[Z] 0.23300E+03 c Pressure 0.76474E-01 10 0.92189E-08 0.28078E+08 0.13948E+03 c k 0.25608E+04 2 0.76749E-06 0.12503E+07 0.55174E+04 c omega 0.81520E+09 1 0.49329E-08 0.52244E+12 0.52922E+02 c TotEner 0.24241E+06 1 0.16902E-05 0.28447E+08 0.58053E+02 c temperature 0.00000E+00 0 0.00000E+00 0.86655E+02 0.75082E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9149e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.08 231.09 0.0013147 0.001357 v Velocity[Y] -0.12979 701.9 250.6 81.156 v Velocity[Z] -19.119 385.81 25.95 1.9966 v ǁVelocityǁ 0.23125 701.9 260.84 83.896 v Pressure 47676 1.1024e+05 1.0332e+05 1.0415e+05 v k 1.1744e-08 46166 922.86 355.42 v omega 155.01 9.6788e+09 1.8462e+08 3.4148e+05 v TotEner 73033 6.295e+05 3.4164e+05 2.4859e+05 v temperature 37.595 533.94 397.59 337.25 v Density 0.37324 6.9311 0.94856 1.09 v TurbVisc 8.7448e-19 0.064065 0.010085 0.028665 v CourantNb 1.2847e-05 44.68 0.40168 0.0076176 v FourierNb 4.5524e-05 199.31 1.8073 0.090797 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 37.974 533.94 401.15 421.58 v Boundary Density 0.37339 6.8885 1.0133 0.90375 v Yplus 0 53.733 2.4865 0.98172 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7989e-05 45.171 0.49192 0.010652 INSTANT 0.159453889E-01 TIME STEP NUMBER 30298 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.746500306E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560817950E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.117704634E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58696E+02 Friction velocity uk : 0.10332E+01 0.58696E+02 Dimensionless distance yplus : 0.20537E-01 0.53896E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.12964E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60149E+03 2 0.23255E-06 0.25671E+03 0.38645E+03 c Velocity[X] 0.73521E+01 c Velocity[Y] 0.10887E+02 c Velocity[Z] 0.23847E+03 c Pressure 0.76479E-01 10 0.94988E-08 0.29161E+08 0.14215E+03 c k 0.25624E+04 2 0.78920E-06 0.12924E+07 0.56076E+04 c omega 0.81520E+09 1 0.45997E-08 0.43424E+12 0.48248E+02 c TotEner 0.24241E+06 1 0.17123E-05 0.29177E+08 0.58792E+02 c temperature 0.00000E+00 0 0.00000E+00 0.88988E+02 0.76086E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9144e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.11 231.12 0.0012934 0.0013585 v Velocity[Y] -0.12979 701.9 250.6 81.157 v Velocity[Z] -19.119 386.04 25.959 1.9969 v ǁVelocityǁ 0.23127 701.9 260.84 83.897 v Pressure 47655 1.1024e+05 1.0332e+05 1.0415e+05 v k 1.1744e-08 46212 923.04 355.42 v omega 155.02 9.6788e+09 1.8462e+08 3.4148e+05 v TotEner 72746 6.295e+05 3.4164e+05 2.4859e+05 v temperature 37.209 533.94 397.59 337.25 v Density 0.37309 6.9749 0.94856 1.09 v TurbVisc 8.7446e-19 0.064065 0.010085 0.028665 v CourantNb 1.2841e-05 44.69 0.40177 0.0076178 v FourierNb 4.553e-05 199.27 1.8071 0.090798 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 37.595 533.94 401.13 421.58 v Boundary Density 0.37324 6.9311 1.0138 0.90385 v Yplus 0 53.896 2.4873 0.98214 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7981e-05 45.179 0.49201 0.010652 INSTANT 0.159456520E-01 TIME STEP NUMBER 30299 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.746202177E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560819373E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.117493295E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58700E+02 Friction velocity uk : 0.10332E+01 0.58700E+02 Dimensionless distance yplus : 0.20537E-01 0.54064E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.12971E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60149E+03 2 0.23265E-06 0.26283E+03 0.39102E+03 c Velocity[X] 0.77811E+01 c Velocity[Y] 0.10911E+02 c Velocity[Z] 0.24414E+03 c Pressure 0.76485E-01 10 0.99363E-08 0.30312E+08 0.14492E+03 c k 0.25640E+04 2 0.81193E-06 0.13375E+07 0.57023E+04 c omega 0.81520E+09 1 0.44824E-08 0.39275E+12 0.45885E+02 c TotEner 0.24241E+06 1 0.17354E-05 0.29939E+08 0.59555E+02 c temperature 0.00000E+00 0 0.00000E+00 0.91408E+02 0.77114E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9139e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.15 231.15 0.0012711 0.0013599 v Velocity[Y] -0.12979 701.9 250.6 81.158 v Velocity[Z] -19.118 386.27 25.967 1.9971 v ǁVelocityǁ 0.23129 701.9 260.85 83.898 v Pressure 47634 1.1024e+05 1.0332e+05 1.0415e+05 v k 1.1744e-08 46259 923.23 355.43 v omega 155.02 9.6788e+09 1.8462e+08 3.4148e+05 v TotEner 72455 6.295e+05 3.4164e+05 2.4859e+05 v temperature 36.815 533.94 397.59 337.25 v Density 0.37294 7.02 0.94856 1.09 v TurbVisc 8.7444e-19 0.064064 0.010086 0.028665 v CourantNb 1.2836e-05 44.7 0.40186 0.007618 v FourierNb 4.5535e-05 199.22 1.8069 0.090799 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 37.209 533.94 401.11 421.58 v Boundary Density 0.37309 6.9749 1.0142 0.90395 v Yplus 0 54.064 2.4881 0.98258 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7974e-05 45.188 0.49209 0.010652 INSTANT 0.159459151E-01 TIME STEP NUMBER 30300 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.745856085E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560820785E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.117274875E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58705E+02 Friction velocity uk : 0.10332E+01 0.58705E+02 Dimensionless distance yplus : 0.20537E-01 0.54235E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.12979E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60149E+03 2 0.23277E-06 0.26917E+03 0.39571E+03 c Velocity[X] 0.82471E+01 c Velocity[Y] 0.10916E+02 c Velocity[Z] 0.25001E+03 c Pressure 0.76490E-01 10 0.92124E-08 0.31534E+08 0.14782E+03 c k 0.25657E+04 2 0.83577E-06 0.13850E+07 0.58006E+04 c omega 0.81520E+09 1 0.43569E-08 0.33373E+12 0.42298E+02 c TotEner 0.24241E+06 1 0.17595E-05 0.30727E+08 0.60334E+02 c temperature 0.00000E+00 0 0.00000E+00 0.93920E+02 0.78166E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9133e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.18 231.18 0.0012476 0.0013613 v Velocity[Y] -0.12979 701.9 250.6 81.159 v Velocity[Z] -19.118 386.5 25.976 1.9974 v ǁVelocityǁ 0.23132 701.9 260.86 83.899 v Pressure 47613 1.1024e+05 1.0331e+05 1.0415e+05 v k 1.1744e-08 46306 923.42 355.43 v omega 155.03 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 72158 6.295e+05 3.4164e+05 2.4859e+05 v temperature 36.414 533.94 397.58 337.25 v Density 0.37278 7.0664 0.94856 1.09 v TurbVisc 8.7443e-19 0.064064 0.010086 0.028666 v CourantNb 1.283e-05 44.711 0.40194 0.0076181 v FourierNb 4.554e-05 199.17 1.8067 0.0908 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 36.815 533.94 401.08 421.57 v Boundary Density 0.37294 7.02 1.0147 0.90406 v Yplus 0 54.235 2.4889 0.98303 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7966e-05 45.196 0.49218 0.010653 INSTANT 0.159461782E-01 TIME STEP NUMBER 30301 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.745462348E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560822194E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.117049065E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58709E+02 Friction velocity uk : 0.10332E+01 0.58709E+02 Dimensionless distance yplus : 0.20537E-01 0.54412E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.12986E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60150E+03 2 0.23290E-06 0.27579E+03 0.40054E+03 c Velocity[X] 0.87540E+01 c Velocity[Y] 0.10931E+02 c Velocity[Z] 0.25610E+03 c Pressure 0.76496E-01 10 0.96349E-08 0.32836E+08 0.15084E+03 c k 0.25674E+04 2 0.86078E-06 0.14351E+07 0.59021E+04 c omega 0.81520E+09 1 0.40410E-08 0.31207E+12 0.40902E+02 c TotEner 0.24241E+06 1 0.17846E-05 0.31549E+08 0.61135E+02 c temperature 0.00000E+00 0 0.00000E+00 0.96530E+02 0.79244E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9128e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.21 231.21 0.0012227 0.0013627 v Velocity[Y] -0.12979 701.9 250.6 81.16 v Velocity[Z] -19.117 386.74 25.985 1.9977 v ǁVelocityǁ 0.23134 701.9 260.86 83.9 v Pressure 47592 1.1024e+05 1.0331e+05 1.0415e+05 v k 1.1743e-08 46354 923.62 355.43 v omega 155.03 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 71855 6.295e+05 3.4164e+05 2.4859e+05 v temperature 36.006 533.94 397.58 337.25 v Density 0.37263 7.1143 0.94855 1.09 v TurbVisc 8.7441e-19 0.064064 0.010086 0.028666 v CourantNb 1.2825e-05 44.721 0.40203 0.0076183 v FourierNb 4.5546e-05 199.13 1.8065 0.090801 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 36.414 533.94 401.06 421.57 v Boundary Density 0.37278 7.0664 1.0151 0.90417 v Yplus 0 54.412 2.4897 0.98348 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7958e-05 45.204 0.49227 0.010653 INSTANT 0.159464413E-01 TIME STEP NUMBER 30302 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.745021332E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560823603E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.116815535E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58714E+02 Friction velocity uk : 0.10332E+01 0.58714E+02 Dimensionless distance yplus : 0.20537E-01 0.54593E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.12994E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60150E+03 2 0.23305E-06 0.28261E+03 0.40546E+03 c Velocity[X] 0.93063E+01 c Velocity[Y] 0.10891E+02 c Velocity[Z] 0.26242E+03 c Pressure 0.76501E-01 10 0.97463E-08 0.34224E+08 0.15399E+03 c k 0.25692E+04 2 0.88704E-06 0.14875E+07 0.60066E+04 c omega 0.81520E+09 1 0.40980E-08 0.31679E+12 0.41210E+02 c TotEner 0.24242E+06 1 0.18108E-05 0.32389E+08 0.61944E+02 c temperature 0.00000E+00 0 0.00000E+00 0.99238E+02 0.80348E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9122e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.24 231.25 0.0011965 0.001364 v Velocity[Y] -0.12979 701.9 250.61 81.161 v Velocity[Z] -19.117 386.97 25.994 1.9979 v ǁVelocityǁ 0.23136 701.9 260.87 83.901 v Pressure 47570 1.1024e+05 1.0331e+05 1.0415e+05 v k 1.1743e-08 46402 923.82 355.43 v omega 155.04 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 71546 6.295e+05 3.4164e+05 2.4859e+05 v temperature 35.589 533.94 397.57 337.25 v Density 0.37247 7.1636 0.94855 1.09 v TurbVisc 8.7439e-19 0.064063 0.010086 0.028666 v CourantNb 1.2819e-05 44.731 0.40212 0.0076185 v FourierNb 4.5551e-05 199.08 1.8062 0.090802 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 36.006 533.94 401.03 421.56 v Boundary Density 0.37263 7.1143 1.0156 0.90428 v Yplus 0 54.593 2.4906 0.98395 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.795e-05 45.213 0.49235 0.010653 INSTANT 0.159467044E-01 TIME STEP NUMBER 30303 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.744533444E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560825011E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.116573938E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58718E+02 Friction velocity uk : 0.10332E+01 0.58718E+02 Dimensionless distance yplus : 0.20537E-01 0.54778E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.13002E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60150E+03 2 0.23322E-06 0.28977E+03 0.41056E+03 c Velocity[X] 0.99087E+01 c Velocity[Y] 0.10884E+02 c Velocity[Z] 0.26897E+03 c Pressure 0.76507E-01 11 0.72911E-08 0.35705E+08 0.15729E+03 c k 0.25710E+04 2 0.91465E-06 0.15427E+07 0.61147E+04 c omega 0.81520E+09 1 0.38795E-08 0.35074E+12 0.43362E+02 c TotEner 0.24242E+06 1 0.18383E-05 0.33275E+08 0.62785E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10206E+03 0.81481E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9117e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.28 231.28 0.001169 0.0013653 v Velocity[Y] -0.12979 701.9 250.61 81.162 v Velocity[Z] -19.116 387.21 26.003 1.9982 v ǁVelocityǁ 0.23138 701.9 260.88 83.902 v Pressure 47548 1.1024e+05 1.0331e+05 1.0415e+05 v k 1.1743e-08 46451 924.02 355.44 v omega 155.04 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 71231 6.295e+05 3.4164e+05 2.4859e+05 v temperature 35.164 533.94 397.57 337.25 v Density 0.37232 7.2144 0.94855 1.09 v TurbVisc 8.7437e-19 0.064063 0.010086 0.028666 v CourantNb 1.2813e-05 44.741 0.40221 0.0076187 v FourierNb 4.5556e-05 199.03 1.806 0.090803 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 35.589 533.94 401.01 421.56 v Boundary Density 0.37247 7.1636 1.0161 0.90439 v Yplus 0 54.778 2.4915 0.98443 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7942e-05 45.221 0.49244 0.010653 INSTANT 0.159469675E-01 TIME STEP NUMBER 30304 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.743999136E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560826417E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.116323905E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58723E+02 Friction velocity uk : 0.10332E+01 0.58723E+02 Dimensionless distance yplus : 0.20537E-01 0.54970E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14424E-01 0.13011E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60151E+03 2 0.23340E-06 0.29723E+03 0.41580E+03 c Velocity[X] 0.10567E+02 c Velocity[Y] 0.10873E+02 c Velocity[Z] 0.27579E+03 c Pressure 0.76513E-01 11 0.76313E-08 0.37290E+08 0.16074E+03 c k 0.25728E+04 2 0.94370E-06 0.16009E+07 0.62264E+04 c omega 0.81520E+09 1 0.32400E-08 0.24269E+12 0.36070E+02 c TotEner 0.24242E+06 1 0.18671E-05 0.34197E+08 0.63649E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10499E+03 0.82644E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9111e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.31 231.31 0.0011401 0.0013665 v Velocity[Y] -0.12979 701.9 250.61 81.163 v Velocity[Z] -19.116 387.45 26.012 1.9984 v ǁVelocityǁ 0.2314 701.9 260.88 83.903 v Pressure 47527 1.1024e+05 1.033e+05 1.0415e+05 v k 1.1743e-08 46501 924.23 355.44 v omega 155.05 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 70910 6.295e+05 3.4164e+05 2.4859e+05 v temperature 34.731 533.94 397.57 337.25 v Density 0.37216 7.2669 0.94855 1.09 v TurbVisc 8.7435e-19 0.064063 0.010086 0.028666 v CourantNb 1.2808e-05 44.752 0.40229 0.0076189 v FourierNb 4.5562e-05 198.99 1.8058 0.090804 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 35.164 533.94 400.99 421.55 v Boundary Density 0.37232 7.2144 1.0166 0.90451 v Yplus 0 54.97 2.4924 0.98492 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7934e-05 45.23 0.49253 0.010654 INSTANT 0.159472306E-01 TIME STEP NUMBER 30305 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.743418905E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560827819E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.116065045E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58728E+02 Friction velocity uk : 0.10332E+01 0.58728E+02 Dimensionless distance yplus : 0.20536E-01 0.55166E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13019E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60151E+03 2 0.23361E-06 0.30503E+03 0.42122E+03 c Velocity[X] 0.11287E+02 c Velocity[Y] 0.10880E+02 c Velocity[Z] 0.28287E+03 c Pressure 0.76519E-01 11 0.84054E-08 0.38986E+08 0.16436E+03 c k 0.25747E+04 2 0.97429E-06 0.16623E+07 0.63420E+04 c omega 0.81520E+09 1 0.39964E-08 0.36139E+12 0.44015E+02 c TotEner 0.24242E+06 1 0.18972E-05 0.35162E+08 0.64541E+02 c temperature 0.00000E+00 0 0.00000E+00 0.10805E+03 0.83838E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9106e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.34 231.34 0.0011098 0.0013677 v Velocity[Y] -0.12979 701.9 250.61 81.164 v Velocity[Z] -19.116 387.69 26.022 1.9987 v ǁVelocityǁ 0.23142 701.9 260.89 83.903 v Pressure 47505 1.1024e+05 1.033e+05 1.0415e+05 v k 1.1742e-08 46550 924.44 355.44 v omega 155.05 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 70582 6.295e+05 3.4164e+05 2.486e+05 v temperature 34.288 533.93 397.56 337.25 v Density 0.372 7.3212 0.94855 1.09 v TurbVisc 8.7433e-19 0.064062 0.010087 0.028666 v CourantNb 1.2802e-05 44.762 0.40238 0.0076191 v FourierNb 4.5567e-05 198.94 1.8056 0.090805 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 34.731 533.94 400.96 421.55 v Boundary Density 0.37216 7.2669 1.0171 0.90463 v Yplus 0 55.166 2.4934 0.98542 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7926e-05 45.238 0.49262 0.010654 INSTANT 0.159474936E-01 TIME STEP NUMBER 30306 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.742793290E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560829205E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.115796942E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58732E+02 Friction velocity uk : 0.10332E+01 0.58732E+02 Dimensionless distance yplus : 0.20536E-01 0.55368E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13028E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60152E+03 2 0.23385E-06 0.31319E+03 0.42682E+03 c Velocity[X] 0.12076E+02 c Velocity[Y] 0.10886E+02 c Velocity[Z] 0.29023E+03 c Pressure 0.76525E-01 11 0.80511E-08 0.40806E+08 0.16815E+03 c k 0.25766E+04 2 0.10065E-05 0.17271E+07 0.64616E+04 c omega 0.81520E+09 1 0.37060E-08 0.31385E+12 0.41018E+02 c TotEner 0.24242E+06 1 0.19288E-05 0.36170E+08 0.65459E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11123E+03 0.85063E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.91e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.37 231.38 0.0010779 0.0013689 v Velocity[Y] -0.12979 701.9 250.61 81.165 v Velocity[Z] -19.115 387.93 26.031 1.999 v ǁVelocityǁ 0.23144 701.9 260.9 83.904 v Pressure 47483 1.1024e+05 1.033e+05 1.0415e+05 v k 1.1742e-08 46601 924.66 355.45 v omega 155.06 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 70247 6.295e+05 3.4164e+05 2.486e+05 v temperature 33.836 533.93 397.56 337.25 v Density 0.37185 7.3772 0.94855 1.09 v TurbVisc 8.7432e-19 0.064062 0.010087 0.028666 v CourantNb 1.2796e-05 44.772 0.40247 0.0076193 v FourierNb 4.5573e-05 198.89 1.8054 0.090806 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 34.288 533.93 400.93 421.54 v Boundary Density 0.372 7.3212 1.0176 0.90476 v Yplus 0 55.368 2.4943 0.98593 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7918e-05 45.247 0.49271 0.010654 INSTANT 0.159477567E-01 TIME STEP NUMBER 30307 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.742122873E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560830575E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.115519155E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58737E+02 Friction velocity uk : 0.10332E+01 0.58737E+02 Dimensionless distance yplus : 0.20536E-01 0.55576E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13037E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60152E+03 2 0.23412E-06 0.32173E+03 0.43259E+03 c Velocity[X] 0.12943E+02 c Velocity[Y] 0.10894E+02 c Velocity[Z] 0.29790E+03 c Pressure 0.76531E-01 11 0.82841E-08 0.42762E+08 0.17213E+03 c k 0.25786E+04 2 0.10406E-05 0.17956E+07 0.65856E+04 c omega 0.81520E+09 1 0.36568E-08 0.34438E+12 0.42967E+02 c TotEner 0.24242E+06 1 0.19619E-05 0.37221E+08 0.66403E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11454E+03 0.86322E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9095e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.41 231.41 0.0010442 0.00137 v Velocity[Y] -0.12979 701.9 250.61 81.166 v Velocity[Z] -19.115 388.17 26.04 1.9992 v ǁVelocityǁ 0.23146 701.9 260.9 83.905 v Pressure 47461 1.1024e+05 1.0329e+05 1.0415e+05 v k 1.1742e-08 46652 924.88 355.45 v omega 155.06 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 69905 6.295e+05 3.4164e+05 2.486e+05 v temperature 33.375 533.93 397.55 337.25 v Density 0.37169 7.4351 0.94855 1.09 v TurbVisc 8.743e-19 0.064062 0.010087 0.028667 v CourantNb 1.279e-05 44.783 0.40256 0.0076195 v FourierNb 4.5578e-05 198.85 1.8052 0.090808 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 33.836 533.93 400.91 421.54 v Boundary Density 0.37185 7.3772 1.0182 0.90489 v Yplus 0 55.576 2.4953 0.98646 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.791e-05 45.255 0.4928 0.010654 INSTANT 0.159480198E-01 TIME STEP NUMBER 30308 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.741408280E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560831928E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.115231213E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58741E+02 Friction velocity uk : 0.10332E+01 0.58741E+02 Dimensionless distance yplus : 0.20536E-01 0.55791E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13046E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60152E+03 2 0.23441E-06 0.33066E+03 0.43855E+03 c Velocity[X] 0.13895E+02 c Velocity[Y] 0.10884E+02 c Velocity[Z] 0.30588E+03 c Pressure 0.76538E-01 11 0.81336E-08 0.44869E+08 0.17632E+03 c k 0.25806E+04 2 0.10765E-05 0.18680E+07 0.67142E+04 c omega 0.81520E+09 1 0.52027E-08 0.43109E+12 0.48073E+02 c TotEner 0.24242E+06 1 0.19966E-05 0.38316E+08 0.67373E+02 c temperature 0.00000E+00 0 0.00000E+00 0.11800E+03 0.87615E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9089e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.44 231.44 0.0010086 0.0013711 v Velocity[Y] -0.12979 701.9 250.61 81.167 v Velocity[Z] -19.114 388.41 26.05 1.9995 v ǁVelocityǁ 0.23148 701.9 260.91 83.906 v Pressure 47439 1.1024e+05 1.0329e+05 1.0415e+05 v k 1.1742e-08 46703 925.1 355.45 v omega 155.07 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 69555 6.295e+05 3.4164e+05 2.486e+05 v temperature 32.903 533.93 397.55 337.25 v Density 0.37153 7.495 0.94855 1.09 v TurbVisc 8.7428e-19 0.064061 0.010087 0.028667 v CourantNb 1.2784e-05 44.793 0.40265 0.0076197 v FourierNb 4.5584e-05 198.8 1.805 0.090809 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 33.375 533.93 400.88 421.53 v Boundary Density 0.37169 7.4351 1.0187 0.90502 v Yplus 0 55.791 2.4963 0.987 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7902e-05 45.264 0.49289 0.010655 INSTANT 0.159482829E-01 TIME STEP NUMBER 30309 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.740650179E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560833254E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.114932616E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58746E+02 Friction velocity uk : 0.10332E+01 0.58746E+02 Dimensionless distance yplus : 0.20536E-01 0.56012E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13055E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60153E+03 2 0.23475E-06 0.34003E+03 0.44471E+03 c Velocity[X] 0.14943E+02 c Velocity[Y] 0.10882E+02 c Velocity[Z] 0.31421E+03 c Pressure 0.76544E-01 11 0.93196E-08 0.47140E+08 0.18073E+03 c k 0.25827E+04 2 0.11145E-05 0.19448E+07 0.68478E+04 c omega 0.81520E+09 1 0.45758E-08 0.34915E+12 0.43263E+02 c TotEner 0.24243E+06 1 0.20331E-05 0.39463E+08 0.68374E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12161E+03 0.88946E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9084e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.47 231.47 0.00097112 0.0013721 v Velocity[Y] -0.12979 701.9 250.61 81.168 v Velocity[Z] -19.114 388.66 26.059 1.9998 v ǁVelocityǁ 0.23151 701.9 260.92 83.907 v Pressure 47417 1.1024e+05 1.0329e+05 1.0415e+05 v k 1.1742e-08 46755 925.33 355.46 v omega 155.07 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 69197 6.295e+05 3.4164e+05 2.486e+05 v temperature 32.42 533.93 397.54 337.25 v Density 0.37137 7.5571 0.94855 1.09 v TurbVisc 8.7427e-19 0.064061 0.010087 0.028667 v CourantNb 1.2778e-05 44.804 0.40274 0.0076198 v FourierNb 4.5589e-05 198.75 1.8047 0.09081 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 32.903 533.93 400.86 421.53 v Boundary Density 0.37153 7.495 1.0193 0.90516 v Yplus 0 56.012 2.4974 0.98756 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7894e-05 45.273 0.49298 0.010655 INSTANT 0.159485460E-01 TIME STEP NUMBER 30310 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.739849280E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560834550E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.114622830E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58751E+02 Friction velocity uk : 0.10332E+01 0.58751E+02 Dimensionless distance yplus : 0.20536E-01 0.56239E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13065E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60153E+03 2 0.23512E-06 0.34988E+03 0.45111E+03 c Velocity[X] 0.16100E+02 c Velocity[Y] 0.10891E+02 c Velocity[Z] 0.32289E+03 c Pressure 0.76551E-01 11 0.92066E-08 0.49596E+08 0.18538E+03 c k 0.25848E+04 2 0.11547E-05 0.20265E+07 0.69868E+04 c omega 0.81520E+09 1 0.46324E-08 0.40620E+12 0.46664E+02 c TotEner 0.24243E+06 1 0.20715E-05 0.40666E+08 0.69408E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12539E+03 0.90315E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9078e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.51 231.51 0.00093157 0.0013731 v Velocity[Y] -0.12979 701.9 250.61 81.169 v Velocity[Z] -19.113 388.91 26.069 2 v ǁVelocityǁ 0.23153 701.9 260.93 83.908 v Pressure 47395 1.1024e+05 1.0329e+05 1.0415e+05 v k 1.1741e-08 46808 925.56 355.46 v omega 155.08 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 68832 6.295e+05 3.4164e+05 2.486e+05 v temperature 31.927 533.93 397.54 337.25 v Density 0.37121 7.6214 0.94855 1.09 v TurbVisc 8.7425e-19 0.06406 0.010088 0.028667 v CourantNb 1.2772e-05 44.814 0.40283 0.00762 v FourierNb 4.5595e-05 198.71 1.8045 0.090811 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 32.42 533.93 400.83 421.52 v Boundary Density 0.37137 7.5571 1.0199 0.9053 v Yplus 0 56.239 2.4985 0.98813 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7885e-05 45.281 0.49307 0.010655 INSTANT 0.159488091E-01 TIME STEP NUMBER 30311 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.739006334E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560835813E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.114301284E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58756E+02 Friction velocity uk : 0.10332E+01 0.58756E+02 Dimensionless distance yplus : 0.20536E-01 0.56474E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13075E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60154E+03 2 0.23554E-06 0.36027E+03 0.45775E+03 c Velocity[X] 0.17378E+02 c Velocity[Y] 0.10929E+02 c Velocity[Z] 0.33196E+03 c Pressure 0.76558E-01 11 0.88659E-08 0.52256E+08 0.19029E+03 c k 0.25870E+04 2 0.11974E-05 0.21134E+07 0.71317E+04 c omega 0.81520E+09 1 0.42696E-08 0.34431E+12 0.42962E+02 c TotEner 0.24243E+06 1 0.21119E-05 0.41935E+08 0.70482E+02 c temperature 0.00000E+00 0 0.00000E+00 0.12933E+03 0.91725E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9073e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.54 231.54 0.00088979 0.001374 v Velocity[Y] -0.12979 701.9 250.61 81.17 v Velocity[Z] -19.113 389.15 26.079 2.0003 v ǁVelocityǁ 0.23155 701.9 260.93 83.909 v Pressure 47373 1.1024e+05 1.0328e+05 1.0415e+05 v k 1.1741e-08 46861 925.8 355.46 v omega 155.08 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 68457 6.295e+05 3.4164e+05 2.486e+05 v temperature 31.422 533.93 397.53 337.25 v Density 0.37105 7.6881 0.94855 1.09 v TurbVisc 8.7423e-19 0.06406 0.010088 0.028667 v CourantNb 1.2766e-05 44.825 0.40293 0.0076202 v FourierNb 4.5601e-05 198.66 1.8043 0.090812 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 31.927 533.93 400.8 421.52 v Boundary Density 0.37121 7.6214 1.0205 0.90544 v Yplus 0 56.474 2.4996 0.98871 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7877e-05 45.29 0.49316 0.010656 INSTANT 0.159490722E-01 TIME STEP NUMBER 30312 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.738122132E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560837047E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.113967370E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58760E+02 Friction velocity uk : 0.10332E+01 0.58760E+02 Dimensionless distance yplus : 0.20536E-01 0.56717E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13085E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60154E+03 2 0.23601E-06 0.37114E+03 0.46460E+03 c Velocity[X] 0.18794E+02 c Velocity[Y] 0.10908E+02 c Velocity[Z] 0.34144E+03 c Pressure 0.76566E-01 11 0.85958E-08 0.55142E+08 0.19547E+03 c k 0.25892E+04 2 0.12426E-05 0.22057E+07 0.72824E+04 c omega 0.81520E+09 1 0.40328E-08 0.31543E+12 0.41121E+02 c TotEner 0.24243E+06 1 0.21543E-05 0.43246E+08 0.71575E+02 c temperature 0.00000E+00 0 0.00000E+00 0.13346E+03 0.93176E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9067e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.57 231.57 0.00084571 0.0013749 v Velocity[Y] -0.12979 701.9 250.61 81.171 v Velocity[Z] -19.113 389.41 26.088 2.0006 v ǁVelocityǁ 0.23157 701.9 260.94 83.91 v Pressure 47350 1.1024e+05 1.0328e+05 1.0415e+05 v k 1.1741e-08 46914 926.04 355.47 v omega 155.09 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 68074 6.295e+05 3.4164e+05 2.486e+05 v temperature 30.905 533.93 397.53 337.25 v Density 0.37088 7.7573 0.94855 1.09 v TurbVisc 8.7421e-19 0.06406 0.010088 0.028667 v CourantNb 1.276e-05 44.835 0.40302 0.0076204 v FourierNb 4.5606e-05 198.61 1.8041 0.090813 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 31.422 533.93 400.77 421.51 v Boundary Density 0.37105 7.6881 1.0211 0.90559 v Yplus 0 56.717 2.5007 0.98931 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7869e-05 45.299 0.49325 0.010656 INSTANT 0.159493353E-01 TIME STEP NUMBER 30313 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.737197509E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560838254E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.113620434E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58765E+02 Friction velocity uk : 0.10332E+01 0.58765E+02 Dimensionless distance yplus : 0.20536E-01 0.56968E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13096E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60154E+03 2 0.23654E-06 0.38263E+03 0.47173E+03 c Velocity[X] 0.20366E+02 c Velocity[Y] 0.10909E+02 c Velocity[Z] 0.35136E+03 c Pressure 0.76573E-01 11 0.85927E-08 0.58283E+08 0.20096E+03 c k 0.25915E+04 2 0.12907E-05 0.23044E+07 0.74398E+04 c omega 0.81520E+09 1 0.37423E-08 0.25958E+12 0.37303E+02 c TotEner 0.24243E+06 1 0.21991E-05 0.44627E+08 0.72710E+02 c temperature 0.00000E+00 0 0.00000E+00 0.13778E+03 0.94672E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9061e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.61 231.61 0.00079905 0.0013756 v Velocity[Y] -0.12979 701.9 250.61 81.171 v Velocity[Z] -19.112 389.66 26.098 2.0009 v ǁVelocityǁ 0.23159 701.9 260.95 83.911 v Pressure 47328 1.1024e+05 1.0328e+05 1.0415e+05 v k 1.1741e-08 46968 926.28 355.47 v omega 155.09 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 67681 6.295e+05 3.4164e+05 2.486e+05 v temperature 30.375 533.93 397.53 337.25 v Density 0.37072 7.8291 0.94856 1.09 v TurbVisc 8.742e-19 0.064059 0.010088 0.028668 v CourantNb 1.2754e-05 44.846 0.40311 0.0076206 v FourierNb 4.5612e-05 198.56 1.8039 0.090814 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 30.905 533.93 400.74 421.5 v Boundary Density 0.37088 7.7573 1.0217 0.90575 v Yplus 0 56.968 2.5019 0.98993 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.786e-05 45.308 0.49334 0.010656 INSTANT 0.159495984E-01 TIME STEP NUMBER 30314 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.736233335E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560839436E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.113259780E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10332E+01 0.58770E+02 Friction velocity uk : 0.10332E+01 0.58770E+02 Dimensionless distance yplus : 0.20536E-01 0.57227E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13106E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60155E+03 2 0.23714E-06 0.39478E+03 0.47915E+03 c Velocity[X] 0.22114E+02 c Velocity[Y] 0.10914E+02 c Velocity[Z] 0.36175E+03 c Pressure 0.76582E-01 11 0.82519E-08 0.61708E+08 0.20678E+03 c k 0.25939E+04 2 0.13418E-05 0.24098E+07 0.76044E+04 c omega 0.81520E+09 1 0.42978E-08 0.34264E+12 0.42858E+02 c TotEner 0.24243E+06 1 0.22463E-05 0.46080E+08 0.73883E+02 c temperature 0.00000E+00 0 0.00000E+00 0.14231E+03 0.96216E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9056e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.64 231.64 0.00074965 0.0013763 v Velocity[Y] -0.12979 701.9 250.61 81.172 v Velocity[Z] -19.112 389.91 26.108 2.0011 v ǁVelocityǁ 0.23161 701.9 260.95 83.912 v Pressure 47305 1.1024e+05 1.0327e+05 1.0415e+05 v k 1.174e-08 47022 926.53 355.48 v omega 155.1 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 67279 6.295e+05 3.4164e+05 2.486e+05 v temperature 29.832 533.93 397.52 337.25 v Density 0.37056 7.9038 0.94856 1.09 v TurbVisc 8.7418e-19 0.064059 0.010088 0.028668 v CourantNb 1.2748e-05 44.857 0.4032 0.0076208 v FourierNb 4.5618e-05 198.51 1.8037 0.090815 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 30.375 533.93 400.71 421.5 v Boundary Density 0.37072 7.8291 1.0224 0.90591 v Yplus 0 57.227 2.5032 0.99057 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7851e-05 45.316 0.49343 0.010656 INSTANT 0.159498615E-01 TIME STEP NUMBER 30315 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.735230524E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560840599E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.112884656E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58775E+02 Friction velocity uk : 0.10331E+01 0.58775E+02 Dimensionless distance yplus : 0.20536E-01 0.57495E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13118E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60155E+03 2 0.23781E-06 0.40762E+03 0.48688E+03 c Velocity[X] 0.24063E+02 c Velocity[Y] 0.10911E+02 c Velocity[Z] 0.37264E+03 c Pressure 0.76590E-01 11 0.79892E-08 0.65452E+08 0.21296E+03 c k 0.25963E+04 2 0.13963E-05 0.25228E+07 0.77767E+04 c omega 0.81520E+09 1 0.47439E-08 0.36222E+12 0.44065E+02 c TotEner 0.24243E+06 1 0.22961E-05 0.47604E+08 0.75095E+02 c temperature 0.00000E+00 0 0.00000E+00 0.14706E+03 0.97810E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.905e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.67 231.68 0.00069737 0.0013769 v Velocity[Y] -0.12979 701.9 250.61 81.173 v Velocity[Z] -19.111 390.17 26.118 2.0014 v ǁVelocityǁ 0.23163 701.9 260.96 83.913 v Pressure 47283 1.1024e+05 1.0327e+05 1.0415e+05 v k 1.174e-08 47077 926.79 355.48 v omega 155.1 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 66866 6.295e+05 3.4164e+05 2.486e+05 v temperature 29.275 533.93 397.52 337.25 v Density 0.37039 7.9816 0.94856 1.09 v TurbVisc 8.7416e-19 0.064059 0.010089 0.028668 v CourantNb 1.2742e-05 44.868 0.4033 0.0076211 v FourierNb 4.5624e-05 198.46 1.8034 0.090817 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 29.832 533.93 400.69 421.49 v Boundary Density 0.37056 7.9038 1.023 0.90608 v Yplus 0 57.495 2.5044 0.99123 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7843e-05 45.325 0.49353 0.010657 INSTANT 0.159501246E-01 TIME STEP NUMBER 30316 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.734190025E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560841751E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.112494259E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58779E+02 Friction velocity uk : 0.10331E+01 0.58779E+02 Dimensionless distance yplus : 0.20535E-01 0.57773E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13129E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60156E+03 2 0.23856E-06 0.42123E+03 0.49494E+03 c Velocity[X] 0.26242E+02 c Velocity[Y] 0.10912E+02 c Velocity[Z] 0.38408E+03 c Pressure 0.76599E-01 11 0.86531E-08 0.69556E+08 0.21954E+03 c k 0.25988E+04 2 0.14544E-05 0.26441E+07 0.79573E+04 c omega 0.81520E+09 1 0.50957E-08 0.51870E+12 0.52732E+02 c TotEner 0.24244E+06 1 0.23487E-05 0.49208E+08 0.76350E+02 c temperature 0.00000E+00 0 0.00000E+00 0.15206E+03 0.99456E+02 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9044e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.71 231.71 0.00064215 0.0013775 v Velocity[Y] -0.12979 701.9 250.61 81.174 v Velocity[Z] -19.111 390.42 26.128 2.0017 v ǁVelocityǁ 0.23165 701.9 260.97 83.914 v Pressure 47260 1.1024e+05 1.0327e+05 1.0415e+05 v k 1.174e-08 47133 927.05 355.48 v omega 155.11 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 66442 6.295e+05 3.4164e+05 2.486e+05 v temperature 28.704 533.93 397.51 337.25 v Density 0.37023 8.0625 0.94856 1.09 v TurbVisc 8.7414e-19 0.064058 0.010089 0.028668 v CourantNb 1.2735e-05 44.878 0.40339 0.0076213 v FourierNb 4.563e-05 198.42 1.8032 0.090818 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 29.275 533.93 400.66 421.49 v Boundary Density 0.37039 7.9816 1.0237 0.90625 v Yplus 0 57.773 2.5057 0.9919 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7834e-05 45.334 0.49362 0.010657 INSTANT 0.159503877E-01 TIME STEP NUMBER 30317 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.733112827E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560842899E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.112087723E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58784E+02 Friction velocity uk : 0.10331E+01 0.58784E+02 Dimensionless distance yplus : 0.20535E-01 0.58061E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13141E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60156E+03 2 0.23941E-06 0.43570E+03 0.50336E+03 c Velocity[X] 0.28682E+02 c Velocity[Y] 0.10919E+02 c Velocity[Z] 0.39609E+03 c Pressure 0.76608E-01 10 0.96522E-08 0.74067E+08 0.22654E+03 c k 0.26014E+04 2 0.15165E-05 0.27746E+07 0.81469E+04 c omega 0.81520E+09 1 0.45105E-08 0.38741E+12 0.45572E+02 c TotEner 0.24244E+06 1 0.24045E-05 0.50901E+08 0.77651E+02 c temperature 0.00000E+00 0 0.00000E+00 0.15731E+03 0.10116E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9039e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.74 231.74 0.00058367 0.0013779 v Velocity[Y] -0.12979 701.9 250.61 81.175 v Velocity[Z] -19.11 390.68 26.139 2.002 v ǁVelocityǁ 0.23167 701.9 260.98 83.915 v Pressure 47237 1.1024e+05 1.0326e+05 1.0415e+05 v k 1.174e-08 47189 927.32 355.49 v omega 155.11 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 66007 6.295e+05 3.4164e+05 2.486e+05 v temperature 28.117 533.93 397.51 337.25 v Density 0.37006 8.1469 0.94856 1.09 v TurbVisc 8.7413e-19 0.064058 0.010089 0.028668 v CourantNb 1.2729e-05 44.889 0.40348 0.0076215 v FourierNb 4.5636e-05 198.37 1.803 0.090819 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 28.704 533.93 400.62 421.48 v Boundary Density 0.37023 8.0625 1.0244 0.90643 v Yplus 0 58.061 2.5071 0.9926 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7825e-05 45.343 0.49371 0.010657 INSTANT 0.159506508E-01 TIME STEP NUMBER 30318 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.731999955E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560844050E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.111664113E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58789E+02 Friction velocity uk : 0.10331E+01 0.58789E+02 Dimensionless distance yplus : 0.20535E-01 0.58359E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13153E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60157E+03 2 0.24038E-06 0.45109E+03 0.51217E+03 c Velocity[X] 0.31422E+02 c Velocity[Y] 0.10928E+02 c Velocity[Z] 0.40874E+03 c Pressure 0.76618E-01 11 0.85465E-08 0.79038E+08 0.23402E+03 c k 0.26040E+04 2 0.15829E-05 0.29152E+07 0.83464E+04 c omega 0.81520E+09 1 0.47602E-08 0.48901E+12 0.51200E+02 c TotEner 0.24244E+06 1 0.24635E-05 0.52684E+08 0.79000E+02 c temperature 0.00000E+00 0 0.00000E+00 0.16284E+03 0.10292E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9033e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.78 231.78 0.00052171 0.0013783 v Velocity[Y] -0.12979 701.9 250.61 81.176 v Velocity[Z] -19.11 390.94 26.149 2.0022 v ǁVelocityǁ 0.23169 701.9 260.99 83.916 v Pressure 47214 1.1024e+05 1.0326e+05 1.0415e+05 v k 1.1739e-08 47246 927.59 355.49 v omega 155.12 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 65560 6.295e+05 3.4164e+05 2.486e+05 v temperature 27.514 533.93 397.5 337.25 v Density 0.3699 8.235 0.94856 1.09 v TurbVisc 8.7411e-19 0.064058 0.010089 0.028668 v CourantNb 1.2723e-05 44.9 0.40358 0.0076217 v FourierNb 4.5642e-05 198.32 1.8028 0.09082 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 28.117 533.93 400.59 421.47 v Boundary Density 0.37006 8.1469 1.0252 0.90662 v Yplus 0 58.359 2.5085 0.99332 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7817e-05 45.352 0.49381 0.010657 INSTANT 0.159509139E-01 TIME STEP NUMBER 30319 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.730852470E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560845215E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.111222425E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58794E+02 Friction velocity uk : 0.10331E+01 0.58794E+02 Dimensionless distance yplus : 0.20535E-01 0.58669E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13166E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60157E+03 2 0.24148E-06 0.46753E+03 0.52141E+03 c Velocity[X] 0.34509E+02 c Velocity[Y] 0.10949E+02 c Velocity[Z] 0.42207E+03 c Pressure 0.76629E-01 11 0.89246E-08 0.84535E+08 0.24203E+03 c k 0.26068E+04 2 0.16542E-05 0.30671E+07 0.85563E+04 c omega 0.81520E+09 1 0.41816E-08 0.34839E+12 0.43216E+02 c TotEner 0.24244E+06 1 0.25261E-05 0.54571E+08 0.80402E+02 c temperature 0.00000E+00 0 0.00000E+00 0.16867E+03 0.10475E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9027e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.81 231.81 0.00045586 0.0013785 v Velocity[Y] -0.12979 701.9 250.61 81.177 v Velocity[Z] -19.11 391.2 26.159 2.0025 v ǁVelocityǁ 0.23171 701.9 260.99 83.917 v Pressure 47191 1.1024e+05 1.0326e+05 1.0415e+05 v k 1.1739e-08 47303 927.86 355.5 v omega 155.12 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 65101 6.295e+05 3.4164e+05 2.486e+05 v temperature 26.893 533.93 397.5 337.26 v Density 0.36973 8.327 0.94857 1.09 v TurbVisc 8.7409e-19 0.064057 0.010089 0.028669 v CourantNb 1.2716e-05 44.911 0.40367 0.0076219 v FourierNb 4.5648e-05 198.27 1.8025 0.090821 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 27.514 533.93 400.56 421.47 v Boundary Density 0.3699 8.235 1.0259 0.90681 v Yplus 0 58.669 2.5099 0.99406 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7808e-05 45.361 0.4939 0.010658 INSTANT 0.159511770E-01 TIME STEP NUMBER 30320 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.729671471E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560846396E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.110761571E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58799E+02 Friction velocity uk : 0.10331E+01 0.58799E+02 Dimensionless distance yplus : 0.20535E-01 0.58991E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13179E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60157E+03 2 0.24272E-06 0.48508E+03 0.53111E+03 c Velocity[X] 0.37993E+02 c Velocity[Y] 0.10949E+02 c Velocity[Z] 0.43614E+03 c Pressure 0.76641E-01 11 0.91763E-08 0.90632E+08 0.25060E+03 c k 0.26096E+04 2 0.17307E-05 0.32316E+07 0.87777E+04 c omega 0.81520E+09 1 0.45532E-08 0.36333E+12 0.44133E+02 c TotEner 0.24244E+06 1 0.25926E-05 0.56559E+08 0.81854E+02 c temperature 0.00000E+00 0 0.00000E+00 0.17482E+03 0.10664E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9021e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.85 231.85 0.00038568 0.0013787 v Velocity[Y] -0.12979 701.9 250.61 81.178 v Velocity[Z] -19.109 391.47 26.17 2.0028 v ǁVelocityǁ 0.23173 701.9 261 83.918 v Pressure 47168 1.1024e+05 1.0325e+05 1.0415e+05 v k 1.1739e-08 47361 928.15 355.5 v omega 155.13 9.6788e+09 1.8462e+08 3.4149e+05 v TotEner 64628 6.295e+05 3.4164e+05 2.486e+05 v temperature 26.255 533.93 397.49 337.26 v Density 0.36956 8.4232 0.94857 1.09 v TurbVisc 8.7407e-19 0.064057 0.01009 0.028669 v CourantNb 1.271e-05 44.922 0.40377 0.0076221 v FourierNb 4.5654e-05 198.22 1.8023 0.090822 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 26.893 533.93 400.53 421.46 v Boundary Density 0.36973 8.327 1.0267 0.90701 v Yplus 0 58.991 2.5115 0.99483 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7799e-05 45.37 0.494 0.010658 INSTANT 0.159514401E-01 TIME STEP NUMBER 30321 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.728458088E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560847588E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.110280374E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58804E+02 Friction velocity uk : 0.10331E+01 0.58804E+02 Dimensionless distance yplus : 0.20535E-01 0.59326E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14423E-01 0.13192E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60158E+03 2 0.24414E-06 0.50389E+03 0.54130E+03 c Velocity[X] 0.41940E+02 c Velocity[Y] 0.10935E+02 c Velocity[Z] 0.45101E+03 c Pressure 0.76653E-01 11 0.92233E-08 0.97417E+08 0.25981E+03 c k 0.26125E+04 2 0.18130E-05 0.34101E+07 0.90117E+04 c omega 0.81520E+09 1 0.39981E-08 0.31058E+12 0.40803E+02 c TotEner 0.24244E+06 1 0.26632E-05 0.58663E+08 0.83362E+02 c temperature 0.00000E+00 0 0.00000E+00 0.18133E+03 0.10861E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9015e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.88 231.88 0.00031069 0.0013787 v Velocity[Y] -0.1298 701.9 250.61 81.179 v Velocity[Z] -19.109 391.73 26.18 2.0031 v ǁVelocityǁ 0.23175 701.9 261.01 83.919 v Pressure 47145 1.1024e+05 1.0325e+05 1.0415e+05 v k 1.1739e-08 47419 928.44 355.51 v omega 155.13 9.6788e+09 1.8463e+08 3.4149e+05 v TotEner 64141 6.295e+05 3.4163e+05 2.486e+05 v temperature 25.597 533.93 397.49 337.26 v Density 0.36939 8.5239 0.94857 1.09 v TurbVisc 8.7406e-19 0.064057 0.01009 0.028669 v CourantNb 1.2703e-05 44.933 0.40387 0.0076224 v FourierNb 4.566e-05 198.17 1.8021 0.090824 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 26.255 533.93 400.5 421.46 v Boundary Density 0.36956 8.4232 1.0275 0.90722 v Yplus 0 59.326 2.513 0.99563 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.779e-05 45.379 0.49409 0.010658 INSTANT 0.159517031E-01 TIME STEP NUMBER 30322 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.727213490E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560848790E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.109777557E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58809E+02 Friction velocity uk : 0.10331E+01 0.58809E+02 Dimensionless distance yplus : 0.20535E-01 0.59674E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13206E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60158E+03 2 0.24576E-06 0.52413E+03 0.55205E+03 c Velocity[X] 0.46421E+02 c Velocity[Y] 0.10948E+02 c Velocity[Z] 0.46676E+03 c Pressure 0.76667E-01 11 0.87108E-08 0.10499E+09 0.26973E+03 c k 0.26155E+04 2 0.19016E-05 0.36045E+07 0.92595E+04 c omega 0.81520E+09 1 0.41187E-08 0.32597E+12 0.41802E+02 c TotEner 0.24244E+06 1 0.27385E-05 0.60900E+08 0.84936E+02 c temperature 0.00000E+00 0 0.00000E+00 0.18822E+03 0.11065E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.901e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.91 231.92 0.00023035 0.0013785 v Velocity[Y] -0.1298 701.9 250.61 81.18 v Velocity[Z] -19.108 392 26.191 2.0034 v ǁVelocityǁ 0.23177 701.9 261.02 83.92 v Pressure 47121 1.1024e+05 1.0325e+05 1.0415e+05 v k 1.1739e-08 47478 928.74 355.51 v omega 155.14 9.6788e+09 1.8463e+08 3.4149e+05 v TotEner 63639 6.295e+05 3.4163e+05 2.486e+05 v temperature 24.92 533.93 397.48 337.26 v Density 0.36922 8.6295 0.94857 1.09 v TurbVisc 8.7404e-19 0.064056 0.01009 0.028669 v CourantNb 1.2697e-05 44.944 0.40396 0.0076226 v FourierNb 4.5666e-05 198.12 1.8019 0.090825 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 25.597 533.93 400.46 421.45 v Boundary Density 0.36939 8.5239 1.0283 0.90744 v Yplus 0 59.674 2.5146 0.99645 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7781e-05 45.389 0.49419 0.010659 INSTANT 0.159519662E-01 TIME STEP NUMBER 30323 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.725938874E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560849996E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.109251736E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58814E+02 Friction velocity uk : 0.10331E+01 0.58814E+02 Dimensionless distance yplus : 0.20535E-01 0.60037E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13221E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60159E+03 2 0.24761E-06 0.54590E+03 0.56340E+03 c Velocity[X] 0.51527E+02 c Velocity[Y] 0.10917E+02 c Velocity[Z] 0.48346E+03 c Pressure 0.76681E-01 11 0.81577E-08 0.11349E+09 0.28043E+03 c k 0.26187E+04 2 0.19974E-05 0.38165E+07 0.95221E+04 c omega 0.81520E+09 1 0.40801E-08 0.30871E+12 0.40681E+02 c TotEner 0.24245E+06 1 0.28187E-05 0.63264E+08 0.86569E+02 c temperature 0.00000E+00 0 0.00000E+00 0.19552E+03 0.11278E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.9004e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.95 231.95 0.0001445 0.0013782 v Velocity[Y] -0.1298 701.9 250.62 81.181 v Velocity[Z] -19.108 392.27 26.202 2.0037 v ǁVelocityǁ 0.23179 701.9 261.02 83.921 v Pressure 47098 1.1024e+05 1.0324e+05 1.0415e+05 v k 1.1738e-08 47538 929.04 355.52 v omega 155.14 9.6788e+09 1.8463e+08 3.4149e+05 v TotEner 63121 6.295e+05 3.4163e+05 2.486e+05 v temperature 24.22 533.93 397.47 337.26 v Density 0.36905 8.7404 0.94858 1.09 v TurbVisc 8.7402e-19 0.064056 0.01009 0.028669 v CourantNb 1.269e-05 44.955 0.40406 0.0076228 v FourierNb 4.5672e-05 198.07 1.8016 0.090826 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 24.92 533.93 400.43 421.44 v Boundary Density 0.36922 8.6295 1.0292 0.90766 v Yplus 0 60.037 2.5163 0.9973 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7772e-05 45.398 0.49429 0.010659 INSTANT 0.159522293E-01 TIME STEP NUMBER 30324 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.724635472E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560851192E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.108701402E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58819E+02 Friction velocity uk : 0.10331E+01 0.58819E+02 Dimensionless distance yplus : 0.20535E-01 0.60416E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13236E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60159E+03 2 0.24975E-06 0.56948E+03 0.57543E+03 c Velocity[X] 0.57363E+02 c Velocity[Y] 0.10918E+02 c Velocity[Z] 0.50120E+03 c Pressure 0.76698E-01 8 0.96442E-08 0.12305E+09 0.29200E+03 c k 0.26219E+04 2 0.21010E-05 0.40488E+07 0.98014E+04 c omega 0.81520E+09 1 0.41605E-08 0.30062E+12 0.40144E+02 c TotEner 0.24245E+06 1 0.29045E-05 0.65790E+08 0.88280E+02 c temperature 0.00000E+00 0 0.00000E+00 0.20329E+03 0.11500E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8998e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -231.98 231.99 5.2763e-05 0.0013778 v Velocity[Y] -0.1298 701.9 250.62 81.182 v Velocity[Z] -19.107 392.54 26.213 2.004 v ǁVelocityǁ 0.23181 701.9 261.03 83.922 v Pressure 47075 1.1024e+05 1.0324e+05 1.0415e+05 v k 1.1738e-08 47598 929.35 355.52 v omega 155.15 9.6788e+09 1.8463e+08 3.4149e+05 v TotEner 62586 6.295e+05 3.4163e+05 2.486e+05 v temperature 23.498 533.93 397.47 337.26 v Density 0.36888 8.857 0.94858 1.09 v TurbVisc 8.74e-19 0.064056 0.010091 0.028669 v CourantNb 1.2684e-05 44.967 0.40416 0.007623 v FourierNb 4.5678e-05 198.02 1.8014 0.090827 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 24.22 533.93 400.39 421.44 v Boundary Density 0.36905 8.7404 1.0301 0.9079 v Yplus 0 60.416 2.5181 0.99819 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7763e-05 45.407 0.49439 0.010659 INSTANT 0.159524924E-01 TIME STEP NUMBER 30325 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.723304544E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560852366E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.108124910E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58824E+02 Friction velocity uk : 0.10331E+01 0.58824E+02 Dimensionless distance yplus : 0.20535E-01 0.60812E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13251E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60160E+03 2 0.25220E-06 0.59507E+03 0.58821E+03 c Velocity[X] 0.64055E+02 c Velocity[Y] 0.10923E+02 c Velocity[Z] 0.52010E+03 c Pressure 0.76716E-01 8 0.96482E-08 0.16081E+09 0.33381E+03 c k 0.26253E+04 2 0.22134E-05 0.43038E+07 0.10099E+05 c omega 0.81520E+09 1 0.40040E-08 0.30592E+12 0.40496E+02 c TotEner 0.24245E+06 2 0.69575E-06 0.85801E+08 0.10082E+03 c temperature 0.00000E+00 0 0.00000E+00 0.24673E+03 0.12669E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8992e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.02 232.02 -4.5636e-05 0.0013771 v Velocity[Y] -0.1298 701.9 250.62 81.183 v Velocity[Z] -19.107 392.81 26.224 2.0043 v ǁVelocityǁ 0.23183 701.9 261.04 83.923 v Pressure 47051 1.1024e+05 1.0324e+05 1.0415e+05 v k 1.1738e-08 47659 929.68 355.53 v omega 155.15 9.6788e+09 1.8463e+08 3.4149e+05 v TotEner 62020 6.295e+05 3.4163e+05 2.486e+05 v temperature 22.732 533.93 397.46 337.26 v Density 0.36871 8.9797 0.94859 1.09 v TurbVisc 8.7399e-19 0.064055 0.010091 0.02867 v CourantNb 1.2677e-05 44.978 0.40426 0.0076233 v FourierNb 4.5684e-05 197.97 1.8012 0.090828 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 23.498 533.93 400.36 421.43 v Boundary Density 0.36888 8.857 1.031 0.90815 v Yplus 0 60.812 2.5199 0.9991 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7753e-05 45.416 0.49448 0.01066 INSTANT 0.159527555E-01 TIME STEP NUMBER 30326 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.721947387E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560853508E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.107520466E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58829E+02 Friction velocity uk : 0.10331E+01 0.58829E+02 Dimensionless distance yplus : 0.20535E-01 0.61225E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13267E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60160E+03 2 0.25571E-06 0.62870E+03 0.60460E+03 c Velocity[X] 0.74700E+02 c Velocity[Y] 0.10924E+02 c Velocity[Z] 0.54308E+03 c Pressure 0.76738E-01 8 0.79535E-08 0.17543E+09 0.34866E+03 c k 0.26288E+04 3 0.19504E-06 0.46151E+07 0.10451E+05 c omega 0.81520E+09 1 0.40427E-08 0.28254E+12 0.38918E+02 c TotEner 0.24245E+06 2 0.69919E-06 0.88770E+08 0.10255E+03 c temperature 0.00000E+00 0 0.00000E+00 0.25610E+03 0.12907E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8986e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.06 232.06 -0.00014434 0.0013765 v Velocity[Y] -0.1298 701.9 250.62 81.184 v Velocity[Z] -19.106 393.08 26.235 2.0046 v ǁVelocityǁ 0.23185 701.9 261.05 83.924 v Pressure 47027 1.1024e+05 1.0323e+05 1.0415e+05 v k 1.1738e-08 47720 930.01 355.54 v omega 155.16 9.6788e+09 1.8463e+08 3.4149e+05 v TotEner 61426 6.295e+05 3.4163e+05 2.486e+05 v temperature 21.928 533.93 397.46 337.26 v Density 0.36854 9.1088 0.94859 1.09 v TurbVisc 8.7397e-19 0.064055 0.010091 0.02867 v CourantNb 1.267e-05 44.989 0.40435 0.0076235 v FourierNb 4.5691e-05 197.92 1.8009 0.090829 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 22.732 533.93 400.32 421.42 v Boundary Density 0.36871 8.9797 1.032 0.90841 v Yplus 0 61.225 2.5218 1.0001 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7744e-05 45.425 0.49458 0.01066 INSTANT 0.159530187E-01 TIME STEP NUMBER 30327 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.720565320E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560854614E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.106857826E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58833E+02 Friction velocity uk : 0.10331E+01 0.58833E+02 Dimensionless distance yplus : 0.20535E-01 0.61657E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13284E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60161E+03 2 0.25985E-06 0.66526E+03 0.62192E+03 c Velocity[X] 0.86659E+02 c Velocity[Y] 0.10940E+02 c Velocity[Z] 0.56766E+03 c Pressure 0.76763E-01 14 0.82028E-08 0.19183E+09 0.36459E+03 c k 0.26325E+04 3 0.20656E-06 0.49266E+07 0.10790E+05 c omega 0.81520E+09 1 0.39640E-08 0.28773E+12 0.39274E+02 c TotEner 0.24245E+06 2 0.70455E-06 0.91964E+08 0.10437E+03 c temperature 0.00000E+00 0 0.00000E+00 0.26613E+03 0.13157E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.898e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.09 232.09 -0.00024485 0.0013758 v Velocity[Y] -0.1298 701.9 250.62 81.185 v Velocity[Z] -19.106 393.36 26.246 2.0049 v ǁVelocityǁ 0.23186 701.9 261.06 83.925 v Pressure 47004 1.1024e+05 1.0323e+05 1.0415e+05 v k 1.1737e-08 47787 930.35 355.54 v omega 155.16 9.6788e+09 1.8463e+08 3.4149e+05 v TotEner 60805 6.295e+05 3.4163e+05 2.486e+05 v temperature 21.088 533.93 397.45 337.26 v Density 0.36837 9.2449 0.9486 1.09 v TurbVisc 8.7395e-19 0.064054 0.010091 0.02867 v CourantNb 1.2664e-05 45 0.40445 0.0076238 v FourierNb 4.5697e-05 197.87 1.8007 0.090831 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 21.928 533.93 400.28 421.41 v Boundary Density 0.36854 9.1088 1.033 0.90868 v Yplus 0 61.657 2.5238 1.001 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7735e-05 45.435 0.49468 0.01066 INSTANT 0.159532818E-01 TIME STEP NUMBER 30328 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.719159691E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560855575E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.106155050E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58838E+02 Friction velocity uk : 0.10331E+01 0.58838E+02 Dimensionless distance yplus : 0.20535E-01 0.62110E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13301E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60161E+03 2 0.26470E-06 0.70517E+03 0.64030E+03 c Velocity[X] 0.10020E+03 c Velocity[Y] 0.10938E+02 c Velocity[Z] 0.59403E+03 c Pressure 0.76792E-01 11 0.97827E-08 0.21039E+09 0.38182E+03 c k 0.26364E+04 3 0.21941E-06 0.52756E+07 0.11158E+05 c omega 0.81520E+09 1 0.38661E-08 0.26375E+12 0.37602E+02 c TotEner 0.24245E+06 2 0.71145E-06 0.95385E+08 0.10630E+03 c temperature 0.00000E+00 0 0.00000E+00 0.27687E+03 0.13420E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8974e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.13 232.13 -0.00034865 0.0013751 v Velocity[Y] -0.1298 701.9 250.62 81.185 v Velocity[Z] -19.106 393.64 26.257 2.0052 v ǁVelocityǁ 0.23188 701.9 261.07 83.926 v Pressure 46980 1.1024e+05 1.0322e+05 1.0415e+05 v k 1.1737e-08 47861 930.7 355.55 v omega 155.17 9.6788e+09 1.8463e+08 3.4149e+05 v TotEner 60158 6.295e+05 3.4163e+05 2.486e+05 v temperature 20.212 533.93 397.45 337.26 v Density 0.36819 9.3891 0.9486 1.09 v TurbVisc 8.7393e-19 0.064054 0.010091 0.02867 v CourantNb 1.2657e-05 45.012 0.40455 0.007624 v FourierNb 4.5703e-05 197.82 1.8005 0.090832 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 21.088 533.93 400.24 421.41 v Boundary Density 0.36837 9.2449 1.034 0.90896 v Yplus 0 62.11 2.5259 1.0021 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7726e-05 45.444 0.49478 0.01066 INSTANT 0.159535449E-01 TIME STEP NUMBER 30329 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.717731878E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560856351E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.105410042E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58843E+02 Friction velocity uk : 0.10331E+01 0.58843E+02 Dimensionless distance yplus : 0.20534E-01 0.62585E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13320E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60162E+03 2 0.27032E-06 0.74897E+03 0.65988E+03 c Velocity[X] 0.11565E+03 c Velocity[Y] 0.10938E+02 c Velocity[Z] 0.62238E+03 c Pressure 0.76826E-01 8 0.85372E-08 0.23161E+09 0.40061E+03 c k 0.26404E+04 3 0.23372E-06 0.56693E+07 0.11559E+05 c omega 0.81520E+09 1 0.38461E-08 0.30908E+12 0.40705E+02 c TotEner 0.24246E+06 2 0.71982E-06 0.99072E+08 0.10833E+03 c temperature 0.00000E+00 0 0.00000E+00 0.28843E+03 0.13698E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8968e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.16 232.16 -0.00045707 0.0013742 v Velocity[Y] -0.1298 701.9 250.62 81.186 v Velocity[Z] -19.105 393.92 26.269 2.0055 v ǁVelocityǁ 0.2319 701.9 261.07 83.927 v Pressure 46956 1.1024e+05 1.0322e+05 1.0415e+05 v k 1.1737e-08 47935 931.06 355.55 v omega 155.17 9.6788e+09 1.8463e+08 3.4149e+05 v TotEner 59486 6.295e+05 3.4163e+05 2.486e+05 v temperature 19.301 533.93 397.44 337.26 v Density 0.36802 9.5423 0.94861 1.09 v TurbVisc 8.7392e-19 0.064053 0.010092 0.02867 v CourantNb 1.265e-05 45.023 0.40466 0.0076243 v FourierNb 4.571e-05 197.76 1.8002 0.090833 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 20.212 533.93 400.19 421.4 v Boundary Density 0.36819 9.3891 1.0351 0.90926 v Yplus 0 62.585 2.5281 1.0032 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7716e-05 45.454 0.49488 0.010661 INSTANT 0.159538080E-01 TIME STEP NUMBER 30330 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.716283282E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560856992E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.104620411E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58848E+02 Friction velocity uk : 0.10331E+01 0.58848E+02 Dimensionless distance yplus : 0.20534E-01 0.63086E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13339E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60162E+03 3 0.11821E-06 0.80600E+03 0.68453E+03 c Velocity[X] 0.13633E+03 c Velocity[Y] 0.11102E+02 c Velocity[Z] 0.65856E+03 c Pressure 0.76866E-01 14 0.80091E-08 0.25621E+09 0.42135E+03 c k 0.26447E+04 3 0.24969E-06 0.61162E+07 0.11997E+05 c omega 0.81520E+09 1 0.37688E-08 0.34172E+12 0.42800E+02 c TotEner 0.24246E+06 2 0.73001E-06 0.10307E+09 0.11050E+03 c temperature 0.00000E+00 0 0.00000E+00 0.30140E+03 0.14002E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8962e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.21 232.21 -0.00058015 0.0013731 v Velocity[Y] -0.1298 701.9 250.62 81.187 v Velocity[Z] -19.105 394.2 26.281 2.0058 v ǁVelocityǁ 0.23192 701.9 261.08 83.928 v Pressure 46932 1.1024e+05 1.0321e+05 1.0415e+05 v k 1.1737e-08 48011 931.43 355.56 v omega 155.18 9.6788e+09 1.8463e+08 3.4149e+05 v TotEner 58786 6.295e+05 3.4163e+05 2.486e+05 v temperature 18.353 533.93 397.43 337.26 v Density 0.36785 9.7055 0.94861 1.09 v TurbVisc 8.739e-19 0.064053 0.010092 0.02867 v CourantNb 1.2643e-05 45.034 0.40476 0.0076246 v FourierNb 4.5716e-05 197.71 1.8 0.090834 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 19.301 533.93 400.15 421.39 v Boundary Density 0.36802 9.5423 1.0363 0.90958 v Yplus 0 63.086 2.5303 1.0043 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7707e-05 45.463 0.49498 0.010661 INSTANT 0.159540711E-01 TIME STEP NUMBER 30331 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.714815340E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560857537E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.103783424E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58854E+02 Friction velocity uk : 0.10331E+01 0.58854E+02 Dimensionless distance yplus : 0.20534E-01 0.63616E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13358E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60163E+03 3 0.11907E-06 0.86018E+03 0.70716E+03 c Velocity[X] 0.15708E+03 c Velocity[Y] 0.11106E+02 c Velocity[Z] 0.69200E+03 c Pressure 0.76915E-01 11 0.98419E-08 0.28474E+09 0.44419E+03 c k 0.26491E+04 3 0.26772E-06 0.66316E+07 0.12482E+05 c omega 0.81520E+09 1 0.38611E-08 0.35713E+12 0.43754E+02 c TotEner 0.24246E+06 2 0.74137E-06 0.10738E+09 0.11278E+03 c temperature 0.00000E+00 0 0.00000E+00 0.31492E+03 0.14313E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8953e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.25 232.25 -0.00071088 0.0013719 v Velocity[Y] -0.1298 701.9 250.62 81.188 v Velocity[Z] -19.104 394.48 26.293 2.0061 v ǁVelocityǁ 0.23194 701.9 261.09 83.929 v Pressure 46908 1.1024e+05 1.0321e+05 1.0415e+05 v k 1.1736e-08 48088 931.81 355.57 v omega 155.18 9.6788e+09 1.8463e+08 3.4149e+05 v TotEner 58058 6.295e+05 3.4163e+05 2.486e+05 v temperature 17.366 533.93 397.43 337.26 v Density 0.36767 9.8799 0.94862 1.09 v TurbVisc 8.7388e-19 0.064053 0.010092 0.02867 v CourantNb 1.2637e-05 45.046 0.40487 0.0076248 v FourierNb 4.5723e-05 197.65 1.7994 0.090835 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 18.353 533.93 400.1 421.38 v Boundary Density 0.36785 9.7055 1.0375 0.90992 v Yplus 0 63.616 2.5328 1.0055 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7697e-05 45.477 0.49512 0.010662 INSTANT 0.159543342E-01 TIME STEP NUMBER 30332 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.713329497E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560857994E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.102884728E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58859E+02 Friction velocity uk : 0.10331E+01 0.58859E+02 Dimensionless distance yplus : 0.20534E-01 0.64177E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13379E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60163E+03 3 0.12017E-06 0.92056E+03 0.73155E+03 c Velocity[X] 0.18119E+03 c Velocity[Y] 0.11103E+02 c Velocity[Z] 0.72826E+03 c Pressure 0.76974E-01 8 0.87421E-08 0.31846E+09 0.46976E+03 c k 0.26539E+04 3 0.28804E-06 0.72224E+07 0.13016E+05 c omega 0.81520E+09 1 0.36468E-08 0.29397E+12 0.39697E+02 c TotEner 0.24246E+06 2 0.75471E-06 0.11214E+09 0.11525E+03 c temperature 0.00000E+00 0 0.00000E+00 0.32977E+03 0.14646E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8945e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.29 232.29 -0.00085039 0.0013704 v Velocity[Y] -0.1298 701.9 250.62 81.189 v Velocity[Z] -19.104 394.77 26.305 2.0064 v ǁVelocityǁ 0.23196 701.9 261.1 83.93 v Pressure 46883 1.1024e+05 1.0321e+05 1.0415e+05 v k 1.1736e-08 48166 932.21 355.58 v omega 155.19 9.6788e+09 1.8463e+08 3.4149e+05 v TotEner 57298 6.295e+05 3.4163e+05 2.486e+05 v temperature 16.336 533.93 397.42 337.26 v Density 0.36749 10.067 0.94863 1.09 v TurbVisc 8.7387e-19 0.064052 0.010092 0.028671 v CourantNb 1.263e-05 45.058 0.40498 0.0076251 v FourierNb 4.5729e-05 197.5 1.7986 0.090836 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 17.366 533.93 400.06 421.37 v Boundary Density 0.36767 9.8799 1.0387 0.91027 v Yplus 0 64.177 2.5353 1.0067 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7688e-05 45.49 0.49524 0.010662 INSTANT 0.159545973E-01 TIME STEP NUMBER 30333 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.711827230E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560858388E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.101931663E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58865E+02 Friction velocity uk : 0.10331E+01 0.58865E+02 Dimensionless distance yplus : 0.20534E-01 0.64772E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13401E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60164E+03 3 0.12149E-06 0.98834E+03 0.75799E+03 c Velocity[X] 0.20949E+03 c Velocity[Y] 0.11111E+02 c Velocity[Z] 0.76773E+03 c Pressure 0.77048E-01 6 0.91934E-08 0.35870E+09 0.49856E+03 c k 0.26589E+04 3 0.31107E-06 0.79031E+07 0.13604E+05 c omega 0.81520E+09 1 0.37426E-08 0.28878E+12 0.39346E+02 c TotEner 0.24246E+06 2 0.77024E-06 0.11742E+09 0.11793E+03 c temperature 0.00000E+00 0 0.00000E+00 0.34617E+03 0.15006E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8937e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.33 232.33 -0.0010002 0.0013687 v Velocity[Y] -0.1298 701.9 250.62 81.19 v Velocity[Z] -19.103 395.06 26.317 2.0067 v ǁVelocityǁ 0.23198 701.9 261.11 83.931 v Pressure 44973 1.1024e+05 1.032e+05 1.0415e+05 v k 1.1736e-08 48245 932.62 355.58 v omega 155.19 9.6788e+09 1.8463e+08 3.4149e+05 v TotEner 56505 6.295e+05 3.4163e+05 2.486e+05 v temperature 15.259 533.93 397.42 337.26 v Density 0.36731 10.268 0.94863 1.09 v TurbVisc 8.7385e-19 0.064052 0.010093 0.028671 v CourantNb 1.2623e-05 45.07 0.40509 0.0076254 v FourierNb 4.5736e-05 197.29 1.7977 0.090838 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 16.336 533.93 400.01 421.36 v Boundary Density 0.36749 10.067 1.04 0.91065 v Yplus 0 64.772 2.538 1.0081 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7678e-05 45.503 0.49536 0.010662 INSTANT 0.159548604E-01 TIME STEP NUMBER 30334 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.710310040E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560858736E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.100920085E-02 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58870E+02 Friction velocity uk : 0.10331E+01 0.58870E+02 Dimensionless distance yplus : 0.20534E-01 0.65406E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13424E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60165E+03 3 0.12303E-06 0.10650E+04 0.78684E+03 c Velocity[X] 0.24303E+03 c Velocity[Y] 0.11123E+02 c Velocity[Z] 0.81086E+03 c Pressure 0.77142E-01 10 0.99757E-08 0.40715E+09 0.53116E+03 c k 0.26643E+04 3 0.33727E-06 0.86906E+07 0.14254E+05 c omega 0.81520E+09 1 0.39282E-08 0.27221E+12 0.38200E+02 c TotEner 0.24246E+06 2 0.78830E-06 0.12331E+09 0.12086E+03 c temperature 0.00000E+00 0 0.00000E+00 0.36438E+03 0.15396E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8929e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.37 232.37 -0.0011623 0.0013666 v Velocity[Y] -0.1298 701.9 250.62 81.191 v Velocity[Z] -19.103 395.35 26.33 2.007 v ǁVelocityǁ 0.232 701.9 261.12 83.932 v Pressure 42525 1.1024e+05 1.032e+05 1.0415e+05 v k 1.1736e-08 48324 933.04 355.59 v omega 155.2 9.6788e+09 1.8463e+08 3.415e+05 v TotEner 55675 6.295e+05 3.4163e+05 2.4861e+05 v temperature 14.131 533.93 397.41 337.26 v Density 0.36713 10.484 0.94864 1.09 v TurbVisc 8.7383e-19 0.064051 0.010093 0.028671 v CourantNb 1.2616e-05 45.082 0.40521 0.0076257 v FourierNb 4.5742e-05 197.07 1.7969 0.090839 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 15.259 533.93 399.96 421.36 v Boundary Density 0.36731 10.268 1.0414 0.91106 v Yplus 0 65.406 2.5409 1.0095 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7669e-05 45.515 0.49548 0.010663 INSTANT 0.159551235E-01 TIME STEP NUMBER 30335 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.708779440E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560859018E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.998452380E-03 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58876E+02 Friction velocity uk : 0.10331E+01 0.58876E+02 Dimensionless distance yplus : 0.20534E-01 0.66081E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13449E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60165E+03 3 0.12482E-06 0.11525E+04 0.81849E+03 c Velocity[X] 0.28314E+03 c Velocity[Y] 0.11139E+02 c Velocity[Z] 0.85819E+03 c Pressure 0.77266E-01 10 0.96239E-08 0.46601E+09 0.56826E+03 c k 0.26700E+04 3 0.36720E-06 0.96064E+07 0.14972E+05 c omega 0.81520E+09 1 0.48907E-08 0.41046E+12 0.46907E+02 c TotEner 0.24247E+06 2 0.80925E-06 0.12992E+09 0.12405E+03 c temperature 0.00000E+00 0 0.00000E+00 0.38470E+03 0.15819E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8922e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.41 232.41 -0.0013387 0.0013642 v Velocity[Y] -0.12981 701.9 250.62 81.192 v Velocity[Z] -19.103 395.64 26.342 2.0073 v ǁVelocityǁ 0.23202 701.9 261.13 83.933 v Pressure 39825 1.1024e+05 1.0319e+05 1.0415e+05 v k 1.1736e-08 48405 933.49 355.6 v omega 155.2 9.6788e+09 1.8463e+08 3.415e+05 v TotEner 54803 6.295e+05 3.4163e+05 2.4861e+05 v temperature 12.946 533.93 397.4 337.26 v Density 0.36695 10.717 0.94865 1.09 v TurbVisc 8.7381e-19 0.064051 0.010093 0.028671 v CourantNb 1.2609e-05 45.095 0.40532 0.007626 v FourierNb 4.5749e-05 196.85 1.7963 0.09084 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 14.131 533.93 399.92 421.35 v Boundary Density 0.36713 10.484 1.0429 0.91149 v Yplus 0 66.081 2.5439 1.0109 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7659e-05 45.527 0.49559 0.010663 INSTANT 0.159553866E-01 TIME STEP NUMBER 30336 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.707236966E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560859247E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.987016667E-03 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58881E+02 Friction velocity uk : 0.10331E+01 0.58881E+02 Dimensionless distance yplus : 0.20534E-01 0.66802E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13475E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60166E+03 3 0.12695E-06 0.12531E+04 0.85347E+03 c Velocity[X] 0.33158E+03 c Velocity[Y] 0.11157E+02 c Velocity[Z] 0.91034E+03 c Pressure 0.77434E-01 14 0.79032E-08 0.53819E+09 0.61068E+03 c k 0.26762E+04 3 0.40153E-06 0.10677E+08 0.15770E+05 c omega 0.81521E+09 1 0.57520E-08 0.52850E+12 0.53227E+02 c TotEner 0.24247E+06 2 0.83356E-06 0.13735E+09 0.12755E+03 c temperature 0.00000E+00 0 0.00000E+00 0.40750E+03 0.16281E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8914e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.45 232.45 -0.001532 0.0013613 v Velocity[Y] -0.12981 701.9 250.62 81.193 v Velocity[Z] -19.102 395.94 26.355 2.0076 v ǁVelocityǁ 0.23204 701.9 261.14 83.934 v Pressure 36831 1.1024e+05 1.0319e+05 1.0415e+05 v k 1.1735e-08 48487 933.94 355.61 v omega 155.21 9.6788e+09 1.8463e+08 3.415e+05 v TotEner 53886 6.295e+05 3.4162e+05 2.4861e+05 v temperature 11.697 533.93 397.4 337.26 v Density 0.36677 10.97 0.94866 1.09 v TurbVisc 8.738e-19 0.06405 0.010094 0.028671 v CourantNb 1.2602e-05 45.107 0.40543 0.0076263 v FourierNb 4.5756e-05 196.66 1.7957 0.090841 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 12.946 533.93 399.87 421.34 v Boundary Density 0.36695 10.717 1.0445 0.91196 v Yplus 0 66.802 2.5471 1.0125 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.7649e-05 45.538 0.49571 0.010663 INSTANT 0.159556497E-01 TIME STEP NUMBER 30337 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.705684168E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560859455E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.974831071E-03 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58887E+02 Friction velocity uk : 0.10331E+01 0.58887E+02 Dimensionless distance yplus : 0.20534E-01 0.67574E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13502E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60166E+03 3 0.12949E-06 0.13699E+04 0.89235E+03 c Velocity[X] 0.39063E+03 c Velocity[Y] 0.11167E+02 c Velocity[Z] 0.96809E+03 c Pressure 0.77670E-01 14 0.83102E-08 0.62758E+09 0.65945E+03 c k 0.26829E+04 3 0.44110E-06 0.11937E+08 0.16658E+05 c omega 0.81521E+09 1 0.52759E-08 0.47940E+12 0.50694E+02 c TotEner 0.24247E+06 2 0.86176E-06 0.14576E+09 0.13140E+03 c temperature 0.00000E+00 0 0.00000E+00 0.43324E+03 0.16787E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8907e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.49 232.49 -0.0017451 0.001358 v Velocity[Y] -0.12981 701.9 250.62 81.194 v Velocity[Z] -19.102 396.24 26.367 2.008 v ǁVelocityǁ 0.23206 701.9 261.15 83.935 v Pressure 33489 1.1024e+05 1.0318e+05 1.0415e+05 v k 1.1735e-08 48569 934.42 355.62 v omega 155.21 9.6788e+09 1.8463e+08 3.415e+05 v TotEner 52917 6.295e+05 3.4162e+05 2.4861e+05 v temperature 10.376 533.93 397.39 337.26 v Density 0.36658 11.244 0.94867 1.09 v TurbVisc 8.7378e-19 0.06405 0.010094 0.028671 v CourantNb 1.2595e-05 45.119 0.40554 0.0076267 v FourierNb 4.5762e-05 196.5 1.7952 0.090843 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 11.697 533.93 399.81 421.33 v Boundary Density 0.36677 10.97 1.0462 0.91246 v Yplus 0 67.574 2.5505 1.0142 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.764e-05 45.549 0.49583 0.010664 INSTANT 0.159559128E-01 TIME STEP NUMBER 30338 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.704122616E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560859648E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.961823589E-03 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58892E+02 Friction velocity uk : 0.10331E+01 0.58892E+02 Dimensionless distance yplus : 0.20534E-01 0.68403E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14422E-01 0.13531E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60167E+03 3 0.13258E-06 0.15068E+04 0.93587E+03 c Velocity[X] 0.46326E+03 c Velocity[Y] 0.11182E+02 c Velocity[Z] 0.10324E+04 c Pressure 0.78020E-01 10 0.98453E-08 0.73950E+09 0.71585E+03 c k 0.26901E+04 3 0.48689E-06 0.13431E+08 0.17651E+05 c omega 0.81521E+09 1 0.54988E-08 0.49758E+12 0.51646E+02 c TotEner 0.24247E+06 2 0.89445E-06 0.15531E+09 0.13564E+03 c temperature 0.00000E+00 0 0.00000E+00 0.46247E+03 0.17345E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.89e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.53 232.53 -0.0019812 0.001354 v Velocity[Y] -0.12981 701.9 250.62 81.195 v Velocity[Z] -19.101 396.53 26.38 2.0083 v ǁVelocityǁ 0.23208 701.9 261.16 83.936 v Pressure 29736 1.1024e+05 1.0317e+05 1.0415e+05 v k 1.1735e-08 48653 934.92 355.63 v omega 155.22 9.6788e+09 1.8463e+08 3.415e+05 v TotEner 51890 6.295e+05 3.4162e+05 2.4861e+05 v temperature 8.9749 533.93 397.38 337.26 v Density 0.3664 11.543 0.94868 1.09 v TurbVisc 8.7377e-19 0.064049 0.010094 0.028672 v CourantNb 1.2588e-05 45.131 0.40565 0.007627 v FourierNb 4.5769e-05 196.36 1.7948 0.090844 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 10.376 533.93 399.76 421.32 v Boundary Density 0.36658 11.244 1.0479 0.913 v Yplus 0 68.403 2.5542 1.0159 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.763e-05 45.56 0.49594 0.010664 INSTANT 0.159561759E-01 TIME STEP NUMBER 30339 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.702553897E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560859821E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.947911248E-03 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10331E+01 0.58898E+02 Friction velocity uk : 0.10331E+01 0.58898E+02 Dimensionless distance yplus : 0.20534E-01 0.69293E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14421E-01 0.13562E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60168E+03 3 0.13637E-06 0.16689E+04 0.98492E+03 c Velocity[X] 0.55344E+03 c Velocity[Y] 0.11192E+02 c Velocity[Z] 0.11043E+04 c Pressure 0.78572E-01 10 0.93337E-08 0.88133E+09 0.78148E+03 c k 0.26980E+04 3 0.54017E-06 0.15215E+08 0.18767E+05 c omega 0.81521E+09 1 0.56150E-08 0.49704E+12 0.51618E+02 c TotEner 0.24247E+06 2 0.93240E-06 0.16623E+09 0.14032E+03 c temperature 0.00000E+00 0 0.00000E+00 0.49593E+03 0.17961E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8894e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.57 232.56 -0.0022445 0.0013494 v Velocity[Y] -0.12981 701.9 250.62 81.196 v Velocity[Z] -19.101 396.84 26.393 2.0086 v ǁVelocityǁ 0.23209 701.9 261.17 83.937 v Pressure 25493 1.1024e+05 1.0317e+05 1.0415e+05 v k 1.1735e-08 48738 935.44 355.64 v omega 155.22 9.6788e+09 1.8463e+08 3.415e+05 v TotEner 50799 6.295e+05 3.4162e+05 2.4861e+05 v temperature 7.4826 533.93 397.37 337.26 v Density 0.36621 11.869 0.94869 1.09 v TurbVisc 8.7375e-19 0.064049 0.010094 0.028672 v CourantNb 1.2581e-05 45.143 0.40576 0.0076274 v FourierNb 4.5776e-05 196.24 1.7944 0.090845 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 8.9749 533.93 399.7 421.31 v Boundary Density 0.3664 11.543 1.0498 0.91358 v Yplus 0 69.293 2.5581 1.0178 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.762e-05 45.571 0.49606 0.010665 INSTANT 0.159564390E-01 TIME STEP NUMBER 30340 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.700979611E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560859989E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.932998131E-03 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10330E+01 0.58903E+02 Friction velocity uk : 0.10330E+01 0.58903E+02 Dimensionless distance yplus : 0.20534E-01 0.70254E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14421E-01 0.13595E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60168E+03 3 0.14104E-06 0.18630E+04 0.10406E+04 c Velocity[X] 0.66648E+03 c Velocity[Y] 0.11225E+02 c Velocity[Z] 0.11853E+04 c Pressure 0.79526E-01 14 0.81923E-08 0.10634E+10 0.85843E+03 c k 0.27066E+04 3 0.60249E-06 0.17368E+08 0.20028E+05 c omega 0.81521E+09 1 0.55756E-08 0.46293E+12 0.49815E+02 c TotEner 0.24247E+06 2 0.97646E-06 0.17880E+09 0.14553E+03 c temperature 0.00000E+00 0 0.00000E+00 0.53454E+03 0.18647E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8887e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.6 232.6 -0.0025396 0.0013441 v Velocity[Y] -0.12981 701.9 250.62 81.197 v Velocity[Z] -19.1 397.14 26.406 2.009 v ǁVelocityǁ 0.23211 701.9 261.18 83.938 v Pressure 20661 1.1024e+05 1.0316e+05 1.0415e+05 v k 1.1734e-08 48824 935.99 355.65 v omega 155.23 9.6788e+09 1.8463e+08 3.415e+05 v TotEner 49635 6.295e+05 3.4162e+05 2.4861e+05 v temperature 5.8868 533.93 397.37 337.26 v Density 0.36603 12.227 0.94871 1.09 v TurbVisc 8.7373e-19 0.064048 0.010095 0.028672 v CourantNb 1.2574e-05 45.155 0.40588 0.0076277 v FourierNb 4.5783e-05 196.13 1.7941 0.090847 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 7.4826 533.93 399.65 421.3 v Boundary Density 0.36621 11.869 1.0518 0.91421 v Yplus 0 70.254 2.5623 1.0199 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.761e-05 45.582 0.49617 0.010665 INSTANT 0.159567021E-01 TIME STEP NUMBER 30341 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.699401373E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560860149E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.916972899E-03 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10330E+01 0.58909E+02 Friction velocity uk : 0.10330E+01 0.58909E+02 Dimensionless distance yplus : 0.20533E-01 0.71292E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14421E-01 0.13630E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ Incoming flow detained for 8 outlet faces on 80 ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60169E+03 3 0.14769E-06 0.25104E+04 0.12079E+04 c Velocity[X] 0.82061E+03 c Velocity[Y] 0.40408E+03 c Velocity[Z] 0.12858E+04 c Pressure 0.81403E-01 14 0.77730E-08 0.12692E+10 0.93782E+03 c k 0.27162E+04 3 0.67572E-06 0.19988E+08 0.21459E+05 c omega 0.81521E+09 1 0.57363E-08 0.41825E+12 0.47350E+02 c TotEner 0.24248E+06 2 0.10159E-05 0.18674E+09 0.14873E+03 c temperature 0.00000E+00 0 0.00000E+00 0.60552E+03 0.19847E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.888e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.64 232.64 -0.002866 0.0013379 v Velocity[Y] -0.12981 701.9 250.62 81.198 v Velocity[Z] -19.1 397.45 26.42 2.0093 v ǁVelocityǁ 0.23213 701.9 261.19 83.939 v Pressure 15119 1.1024e+05 1.0316e+05 1.0415e+05 v k 1.1734e-08 48911 936.57 355.66 v omega 155.23 9.6788e+09 1.8463e+08 3.415e+05 v TotEner 48387 6.295e+05 3.4162e+05 2.4861e+05 v temperature 4.1728 533.93 397.36 337.26 v Density 0.36584 12.622 0.94872 1.09 v TurbVisc 8.7372e-19 0.064048 0.010095 0.028672 v CourantNb 1.2567e-05 45.167 0.40599 0.0076281 v FourierNb 4.579e-05 196.04 1.7938 0.090848 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 5.8868 533.93 399.59 421.28 v Boundary Density 0.36603 12.227 1.054 0.91489 v Yplus 0 71.292 2.5668 1.022 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.76e-05 45.592 0.49629 0.010666 INSTANT 0.159569653E-01 TIME STEP NUMBER 30342 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.697820801E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560860289E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.887564616E-03 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10330E+01 0.58914E+02 Friction velocity uk : 0.10330E+01 0.58914E+02 Dimensionless distance yplus : 0.20533E-01 0.72420E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14421E-01 0.13667E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ Incoming flow detained for 16 outlet faces on 80 ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60170E+03 3 0.15927E-06 0.32647E+04 0.13775E+04 c Velocity[X] 0.12286E+04 c Velocity[Y] 0.61617E+03 c Velocity[Z] 0.14199E+04 c Pressure 0.86002E-01 12 0.97283E-08 0.15538E+10 0.10376E+04 c k 0.27269E+04 3 0.76585E-06 0.24863E+08 0.23902E+05 c omega 0.81521E+09 1 0.57239E-08 0.43477E+12 0.48277E+02 c TotEner 0.24248E+06 2 0.10665E-05 0.20189E+09 0.15464E+03 c temperature 0.00000E+00 0 0.00000E+00 0.66282E+03 0.20764E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8873e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.68 232.68 -0.003234 0.0013308 v Velocity[Y] -0.12981 701.9 250.62 81.199 v Velocity[Z] -19.1 397.75 26.433 2.0096 v ǁVelocityǁ 0.23215 701.9 261.2 83.94 v Pressure 8709.2 1.1024e+05 1.0315e+05 1.0415e+05 v k 1.1734e-08 48999 937.21 355.68 v omega 155.24 9.6788e+09 1.8463e+08 3.415e+05 v TotEner 47045 6.295e+05 3.4162e+05 2.4861e+05 v temperature 2.3233 533.93 397.35 337.26 v Density 0.36565 13.059 0.94874 1.09 v TurbVisc 8.737e-19 0.064047 0.010094 0.028672 v CourantNb 1.2559e-05 45.179 0.40611 0.0076286 v FourierNb 4.5797e-05 195.94 1.7934 0.090847 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 4.1728 533.93 399.54 421.27 v Boundary Density 0.36584 12.622 1.0564 0.91564 v Yplus 0 72.42 2.5717 1.0244 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.759e-05 45.603 0.4964 0.010666 INSTANT 0.159572284E-01 TIME STEP NUMBER 30343 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.696239529E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560860412E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.858091698E-03 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10330E+01 0.58920E+02 Friction velocity uk : 0.10330E+01 0.58920E+02 Dimensionless distance yplus : 0.20533E-01 0.73648E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14421E-01 0.13707E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ Incoming flow detained for 16 outlet faces on 80 ** INFORMATION ON CONVERGENCE -------------------------- ----------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual ----------------------------------------------------------------------------- c Velocity 0.60170E+03 3 0.16870E-06 0.35304E+04 0.14324E+04 c Velocity[X] 0.16706E+04 c Velocity[Y] 0.30028E+03 c Velocity[Z] 0.15595E+04 c Pressure 0.10349E+00 9 0.91987E-08 0.19762E+10 0.11702E+04 c k 0.27391E+04 3 0.87827E-06 0.30770E+08 0.26553E+05 c omega 0.81521E+09 1 0.81411E-08 0.48945E+12 0.51223E+02 c TotEner 0.24248E+06 2 0.11413E-05 0.23152E+09 0.16560E+03 c temperature 0.00000E+00 0 0.00000E+00 0.71893E+03 0.21625E+03 c Wall distance 0.00000E+00 0 0.00000E+00 0.00000E+00 0.00000E+00 ----------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - --------------- -------------- -------------- ------------ ------------ a k a omega a TotEner a temperature a Local Time Step 2.8867e-09 50160 ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ------------- -------------- -------------- -------------- -------------- v Velocity[X] -232.72 232.72 -0.003659 0.0013222 v Velocity[Y] -0.12981 701.9 250.62 81.199 v Velocity[Z] -19.099 398.06 26.447 2.01 v ǁVelocityǁ 0.23217 701.9 261.21 83.941 v Pressure 1234.3 1.1024e+05 1.0314e+05 1.0415e+05 v k 1.1734e-08 49088 937.92 355.69 v omega 155.24 9.6788e+09 1.8463e+08 3.415e+05 v TotEner 45593 6.295e+05 3.4162e+05 2.4861e+05 v temperature 0.31744 533.93 397.34 337.26 v Density 0.36547 13.546 0.94876 1.09 v TurbVisc 8.7368e-19 0.064047 0.010093 0.028672 v CourantNb 1.2552e-05 45.191 0.40622 0.007629 v FourierNb 4.5804e-05 195.86 1.793 0.090846 v Wall distance 3.6512e-07 0.029499 0.0075674 0.013764 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - -------------------- -------------- -------------- -------------- -------------- v Boundary temperature 2.3233 533.93 399.49 421.26 v Boundary Density 0.36565 13.059 1.0589 0.91647 v Yplus 0 73.648 2.577 1.0269 ** Computed values on cells ------------------------ criterion minimum maximum set mean spatial mean ---------- -------------- -------------- -------------- -------------- CFL / Mass 1.758e-05 45.613 0.49652 0.010667 INSTANT 0.159574915E-01 TIME STEP NUMBER 30344 ============================================================= ** BOUNDARY MASS FLOW INFORMATION ------------------------------ --------------------------------------------------------------- Boundary type Code Nb faces Mass flow --------------------------------------------------------------- Sub. enth. inlet 11 0 0.000000000E+00 Ptot, Htot 10 0 0.000000000E+00 Imp inlet/outlet 7 480 -0.694659202E-04 Subsonic outlet 9 0 0.000000000E+00 Supersonic outlet 8 0 0.000000000E+00 Wall 5 1416 0.560860515E-20 Symmetry 4 0 0.000000000E+00 Undefined 1 0 0.000000000E+00 User type 3 80 0.841762007E-03 --------------------------------------------------------------- ** BOUNDARY CONDITIONS FOR SMOOTH WALLS --------------------------------------- ------------------------------------------------------------ Minimum Maximum ------------------------------------------------------------ Rel velocity at the wall uiptn : 0.00000E+00 0.00000E+00 Friction velocity uet : 0.10330E+01 0.58925E+02 Friction velocity uk : 0.10330E+01 0.58925E+02 Dimensionless distance yplus : 0.20533E-01 0.74991E+02 Friction thermal sca. tstar : 0.00000E+00 0.00000E+00 Dim-less thermal sca. tplus : 0.14421E-01 0.13750E+02 ------------------------------------------------------ Nb of reversal of the velocity at the wall : 0 Nb of faces within the viscous sub-layer : 1416 Total number of wall faces : 1416 ------------------------------------------------------------ Incoming flow detained for 20 outlet faces on 80 /home/ruonanwang/code_saturne_master_git/code_saturne-master/src/cfbl/cs_cf_thermo.c:248: Fatal error. Error in thermodynamics computations for compressible flows : Negative values of the internal energy were encountered in 4 cells. Call stack: 1: 0x7f8030b6aa23 (libsaturne-7.1.so) 2: 0x7f8030b602ac (libsaturne-7.1.so) 3: 0x7f80306958e0 (libsaturne-7.1.so) 4: 0x7f80306a0217 (libsaturne-7.1.so) 5: 0x7f80305112ef (libsaturne-7.1.so) 6: 0x7f80315fb9aa (libcs_solver-7.1.so) 7: 0x7f802f909b97 <__libc_start_main+0xe7> (libc.so.6) 8: 0x5606f87cdd7a <_start+0x2a> (cs_solver) End of stack