command: ./cs_solver *************************************************************** (R) code_saturne Version 9.1-alpha Copyright (C) 1998-2025 EDF S.A., France build mar. 18 mars 2025 14:20:11 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: mer. 30 avril 2025 11:27:49 System: Linux 6.1.0-31-amd64 (Debian GNU/Linux 12 (bookworm)) Machine: dsp1077190 Processor: model name : 11th Gen Intel(R) Core(TM) i7-11850H @ 2.50GHz Memory: 31761 MB User: bj46cd4l (BAPTISTE JEANSELME) Directory: /home/bj46cd4l/Bureau/test/ALE/test_TEST/RESU/e03 OpenMP threads: 5 Processors/node: 16 Compilers used for build: C compiler: gcc (Debian 12.2.0-14) 12.2.0 C++ compiler: g++ (Debian 12.2.0-14) 12.2.0 Fortran compiler: GNU Fortran (Debian 12.2.0-14) 12.2.0 OpenMP version: 4.5 =============================================================== CALCULATION PREPARATION ======================= =============================================================== Read notebook variables from checkpoint: restart/main.csc No error detected during the data verification. Reading file: restart/mesh_input.csm Finished reading: restart/mesh_input.csm Number of cells: 12230 ---------------------------------------------------------- Number of cells + halo cells: 12230 ---------------------------------------------------------- Number of interior faces: 24170 ---------------------------------------------------------- Number of boundary faces: 25038 ---------------------------------------------------------- Histogram of the number of interior faces per cell: minimum value = 2 maximum value = 4 1 : [ 2 ; 3 [ = 4 2 : [ 3 ; 4 ] = 12226 ---------------------------------------------------------- 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: 12230 Numbering for interior faces: type: threads number of threads: 5 number of exclusive groups: 6 number of elements in group 0: 8551 number of elements in group 1: 7539 number of elements in group 2: 4598 number of elements in group 3: 2366 number of elements in group 4: 932 number of elements in group 5: 184 estimated thread imbalance: 0.214 Numbering for boundary faces: type: threads number of threads: 5 number of exclusive groups: 1 number of elements in group 0: 25038 estimated thread imbalance: 0.000 ---------------------------------------------------------- Matrix bandwidth for volume mesh : 12074 Matrix profile/lines for volume mesh : 5691 Mesh coordinates: minimum and maximum X : -5.0000000e+00 5.0000000e+00 Y : -1.1000000e+01 0.0000000e+00 Z : 0.0000000e+00 1.0000000e-01 Mesh Number of cells: 12230 Number of interior faces: 24170 Number of boundary faces: 25038 Number of vertices: 25036 Groups: "1" boundary faces: 49 "2" boundary faces: 378 "3" boundary faces: 24460 "4" boundary faces: 102 "5" interior faces: 49 boundary faces: 49 "6" cells: 12230 "inlet" boundary faces: 49 "outlet" interior faces: 49 boundary faces: 49 "plaque" boundary faces: 378 "symetrie_z" boundary faces: 24460 "vol" cells: 12230 "walls" boundary faces: 102 --- Information on the volumes Minimum control volume = 1.1671193e-06 Maximum control volume = 1.2244898e-02 Total volume for the domain = 1.0995000e+01 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 (0.00561 s) --- Information on volume zones Volume zone "cells" id = 0 Number of cells = 12230 Volume = 10.995 Center of gravity = (-9.1388e-07, -5.501, 0.05) Volume zone "all_cells" id = 1 Number of cells = 12230 Volume = 10.995 Center of gravity = (-9.1388e-07, -5.501, 0.05) --- Information on boundary zones Boundary zone "boundary_faces" id = 0 Number of faces = 25038 Surface = 224.31 Center of gravity = (-1.3463e-16, -5.4989, 0.05) Boundary zone "inlet" id = 1 Number of faces = 49 Surface = 1 Center of gravity = (-6.9389e-18, 0, 0.05) Boundary zone "plaque" id = 2 Number of faces = 378 Surface = 0.21 Center of gravity = (1.2326e-17, -3.3333, 0.05) Boundary zone "sym" id = 3 Number of faces = 24460 Surface = 219.9 Center of gravity = (-2.1609e-16, -5.501, 0.05) Boundary zone "walls" id = 4 Number of faces = 102 Surface = 2.2 Center of gravity = (0, -5.5, 0.05) Boundary zone "outlet" id = 5 Number of faces = 49 Surface = 1 Center of gravity = (-2.7756e-17, -11, 0.05) Characteristic values for turbulence: ------------------------------------- almax: 2.22 (characteristic length for initialization) Restart: -------- Start reading from restart/main.csc Reading dimensions complete Restart time information nt_prev = 200 t_prev = 2.0000e+00 Reading options complete Read variables from: restart/main.csc Start reading from restart/auxiliary.csc Finished reading options. restart/auxiliary.csc: section "ref_presstot01" not present. Finished reading physical properties. Finished reading boundary conditions. Finished reading source terms. 1269 faces have a too small distance between centers. For these faces, the weight may be clipped. 1541 boundary faces have a too small distance between cell center and face center. --- Information on the volumes Minimum control volume = -1.3971645e-05 Maximum control volume = 1.2244898e-02 Total volume for the domain = 1.0995000e+01 Abort due to the detection of a negative control volume. Finished reading ALE information. -------------------------------------------------------------------------------- ** VARIABLES INITIALIZATION ------------------------ ----------------------------------------- Property Min. value Max. value ----------------------------------------- density 1.1786e+00 1.1786e+00 molecular_viscos 1.8300e-05 1.8300e-05 turbulent_viscos 1.3511e-06 6.4246e-02 ----------------------------------------- ** Information on boundary faces type ---------------------------------- -------------------------------------------------------------------------------- Boundary type Code Nb faces -------------------------------------------------------------------------------- Inlet 2 0 Smooth wall 5 378 Rough wall 6 0 Symmetry 4 24660 Free outlet 3 0 Free inlet 14 0 Convective inlet 16 0 Free surface 64 0 Undefined 1 0 -------------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ------- -------------- -------------- ------------ ------------ a k a epsilon ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.037554 0.036429 -4.9958e-05 2.5136e-07 v Velocity[Y] -0.025199 0.021013 0.0039878 -5.8118e-06 v Velocity[Z] -2.0436e-17 1.218e-17 2.8169e-20 9.93e-23 v ǁVelocityǁ 5.9874e-06 0.038268 0.0060537 0.00060285 v Pressure -0.0031695 0.0022363 6.7879e-06 -1.6444e-07 v k 1.186e-05 0.00061226 0.00049404 0.00059785 v epsilon 5.9259e-07 0.00060166 4.4777e-06 6.373e-07 v Mesh Velocity[X] 0 0 0 0 v Mesh Velocity[Y] 4.0344e-06 0.012711 0.007285 0.0017507 v Mesh Velocity[Z] 0 0 0 0 v ǁMesh Velocityǁ 4.0344e-06 0.012711 0.007285 0.0017507 v TurbVisc 1.3511e-06 0.064246 0.038238 0.06339 v CourantNb 0 0 0 0 v FourierNb 0 0 0 0 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v mesh_vi1 1 1 1 1 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ------------------ -------------- -------------- -------------- -------------- v boundary_stress[X] 0 0 0 0 v boundary_stress[Y] 0 0 0 0 v boundary_stress[Z] 0 0 0 0 v ǁboundary_stressǁ 0 0 0 0 v Yplus 0 0 0 0 ** Field values on vertices ------------------------ field minimum maximum set mean - -------------------- -------------- -------------- -------------- v Mesh displacement[X] 0 0 0 v Mesh displacement[Y] 0 0.029389 0.0058241 v Mesh displacement[Z] 0 0 0 v ǁMesh displacementǁ 0 0.029389 0.0058241 =============================================================== MAIN CALCULATION ================ =============================================================== -------------------------------------------------------------------------------- Write final restart files Checkpoint at iteration 200, physical time 2.00000 ** Writing the main restart file ----------------------------- Start writing Wrote field names and types to checkpoint at iteration 200: checkpoint/main.csc End writing the options Wrote main variables to checkpoint: checkpoint/main.csc Wrote notebook variables to checkpoint: checkpoint/main.csc End writing ** Writing the auxiliary restart file ---------------------------------- Start writing End writing the dimensions and options End writing the physical properties End writing the time step Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary.csc End writing the ALE data End writing ** Information on convergence -------------------------- -------------------------------------------------------------------------------- Variable Rhs norm N_iter Norm. residual Drift Time residual -------------------------------------------------------------------------------- -------------------------------------------------------------------------------- ** Clippings for computed fields ----------------------------- field initial min initial max clips to min clips to max - ------- -------------- -------------- ------------ ------------ a k a epsilon ** Field values on cells --------------------- field minimum maximum set mean spatial mean - ---------------- -------------- -------------- -------------- -------------- v Velocity[X] -0.037554 0.036429 -4.9958e-05 2.5136e-07 v Velocity[Y] -0.025199 0.021013 0.0039878 -5.8118e-06 v Velocity[Z] -2.0436e-17 1.218e-17 2.8169e-20 9.93e-23 v ǁVelocityǁ 5.9874e-06 0.038268 0.0060537 0.00060285 v Pressure -0.0031695 0.0022363 6.7879e-06 -1.6444e-07 v k 1.186e-05 0.00061226 0.00049404 0.00059785 v epsilon 5.9259e-07 0.00060166 4.4777e-06 6.373e-07 v Mesh Velocity[X] 0 0 0 0 v Mesh Velocity[Y] 4.0344e-06 0.012711 0.007285 0.0017507 v Mesh Velocity[Z] 0 0 0 0 v ǁMesh Velocityǁ 4.0344e-06 0.012711 0.007285 0.0017507 v TurbVisc 1.3511e-06 0.064246 0.038238 0.06339 v CourantNb 0 0 0 0 v FourierNb 0 0 0 0 v total_pressure 1.0132e+05 1.0133e+05 1.0132e+05 1.0132e+05 v mesh_vi1 1 1 1 1 v volume_forces[X] 0 0 0 0 v volume_forces[Y] 0 0 0 0 v volume_forces[Z] 0 0 0 0 v ǁvolume_forcesǁ 0 0 0 0 ** Field values on boundary_faces ------------------------------ field minimum maximum set mean spatial mean - ------------------ -------------- -------------- -------------- -------------- v boundary_stress[X] 0 0 0 0 v boundary_stress[Y] 0 0 0 0 v boundary_stress[Z] 0 0 0 0 v ǁboundary_stressǁ 0 0 0 0 v Yplus 0 0 0 0 ** Field values on vertices ------------------------ field minimum maximum set mean - -------------------- -------------- -------------- -------------- v Mesh displacement[X] 0 0 0 v Mesh displacement[Y] 0 0.029389 0.0058241 v Mesh displacement[Z] 0 0 0 v ǁMesh displacementǁ 0 0.029389 0.0058241 =============================================================== FINAL STAGE OF THE CALCULATION ============================== =============================================================== =============================================================== END OF CALCULATION ================== =============================================================== Destroying structures and ending computation